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  • Berlin  (37)
  • United States Congress  (37)
  • United States National Advisory Committee for Aeronautics  (10)
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  • 1
    UID:
    gbv_75524317X
    Format: Online-Ressource (80 p) , tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2009 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 13299
    Note: Additional views of Hon. Joseph L. Fisher, p. 75 , Dissenting views of Hon. J.J. Pickle, p. 70 , Minority views by Hon. Bill Frenzel, p. 76 , Separate views of Hon. Andy Jacobs, Jr, p. 72 , Table of contents, p. III , © 2009 by NewsBank, Inc. All rights reserved
    Language: English
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  • 2
    UID:
    gbv_681926007
    Format: Online-Ressource (10 p)
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2005 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 2067
    Note: Views of the minority, p. 5 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
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  • 3
    UID:
    gbv_681694041
    Format: Online-Ressource (656 p) , illustrations, maps, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2004 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 1122
    Note: A few words on horses, by Ruth Hall, p. 544 , Agriculture of San Bernardino County, Cal., by Lionel M. Jacobs, p. 157 , Artificial manures, by Professor C. Upham Sheppard, p. 144 , Belt of no frost, or thermal belt, by Silas M'Dowell, p. 146 , Character, cultivation, and use of the lupine, by Louis Schade, p. 370 , Cotton in Missouri, by W.H. Horner, p. 221 , Entomology and its relations to the vegetable productions of the soil, with reference to both destructive and beneficial insects, by S.S. Rathvon, p. 585 , Experiments on grape cuttings received from the Patent Office, by S.J. Parker, p. 476 , Farming in the New England states, by James P. Gunnell, p. 251 , Food, qualities and changes requisite to health and strength, by Professor L.C. Loomis, A.M., p. 358 , Fruit culture, by J.K. Eshelman, p. 541 , Grape culture, by Dr. George Pepper Norris, p. 486 , Grape-vine culture and wine-making, by John F. Weber, p. 506 , Grapes on Kelley's Island, Ohio, by George C. Huntington, p. 470 , Hog cholera, by Edwin M. Snow, M.D., p. 147 , Hop culture, by L.T. Marshall, p. 289 , Index follows p. 648 , Indian corn, by Lewis Bollman, p. 262 , List of errata, p. 656 , Notes on the recent progress of agricultural science, by David A. Wells, p. 314 , On the destruction of noxious insects by means of the "Pyrethrum willemoti" duchartre, translated from the French by [i.e., of] C. Willemot, p. 223 , On the fruits of Cabul and vicinity, with a view to the introduction of the grape-vine of that region into the central climate of the United States, by Josiah Harlan, p. 526 , Orchard houses, by Dr. George Pepper Norris, p. 538 , Raising sheep and wool-growing, by W.S. Calohan, p. 119 , Raspberry culture, by J.A. Warder, p. 165 , Remarks on grape culture, with reference to mildew, both on the native and foreign varieties, by William Saunders, p. 495 , Salt marshes, the mode of reclaiming them and their value, by Wm. Clift, p. 343 , Sandomir wheat, by Cichocki, p. 334 , Select breeds of cattle, and their adaptation to the United States, by Francis M. Rotch, p. 427 , Sheep and wool of Steuben County, N.Y., by T.M. Younglove, p. 137 , Sheep-breeding, by Joseph Cape, p. 128 , Sorghum culture and sugar making, by Isaac A. Hedges, p. 293 , Strawberries, by J.A. Warder, p. 175 , Territory of Colorado: its soil -- its climate -- its mineral products and resources, by Edward Bliss, p. 154 , The breeds of sheep best adapted to New England, with suggestions as to their treatment, by Richard S. Tray [i.e., Fay], p. 130 , The consumption of milk, by Silas L. Loomis, A.M., M.D., p. 209 , The culture and manufacture of flax and hemp, by O.S. Leavitt, p. 83 , The culture and manufacture of sugar from sorghum, by D.M. Cook, p. 311 , The dairy farming region of Greene and Orange counties, New York, with some account of the farm of the writer, by Zadock Pratt, p. 411 , The grapes of North America, by S.B. Buckley, p. 478 , The history, industry, and commerce of flax, by D.J. Browne follows p. 20 , The horses of New England, by C.L. Flint, p. 382 , The pear orchard, by John A. Warder, p. 232 , The strawberry -- (Fragaria:) its species, native localities, and their normal sexual character, by William K. Prince, p. 189 , Tropical Florida, by L.D. Stickney, p. 402 , Wheat-growing in Prussia, p. 404 , Wool-growing, by Robert George, p. 124 , Worn-out lands of New Jersey, by Charles Stokes, p. 206 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
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  • 4
    UID:
    gbv_754063038
    Format: Online-Ressource (645 p) , illustrations, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 9802
    Note: A comparison between the theoretical and measured longitudinal stability characteristics of an airplane, by Hartley A. Soule and John B. Wheatley [No. 442], p. 53 , A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests, by Nathan F. Schudder [No. 441], p. 37 , Aircraft power-plant instruments, by Harcourt Sontag and W.G. Brombacher [No. 466], p. 447 , Airfoil section characteristics as affected by protuberances, by Eastman N. Jacobs [No. 446], p. 109 , Appendix, p. 65 , Determination of the theoretical pressure distribution for twenty airfoils, by I.E. Garrick [No. 465], p. 433 , General potential theory of arbitrary wing sections, by T. Theodorsen and I.E. Garrick [No. 452], p. 177 , Improved apparatus for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. and H.L. Dryden [No. 448], p. 131 , Increasing the air charge and scavenging the clearance volume of a compression-ignition engine, by J.S. Spanogle, C.W. Hicks, and H.H. Foster [No. 469], p. 525 , Interference on an airfoil of finite span in an open rectangular wind tunnel, by Theodore Theodoresen [No. 561], p. 355 , List of technical reports, p. VII , Maneuverability investigation of O3U-1 observation airplane, by F.L. Thompson and H.W. Kirschbaum [No. 457], p. 263 , Negative thrust and torque characteristics of an adjustable-pitch metal propeller, by Edwin P. Hartmen [No 464], p. 421 , Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 474], p. 603 , Penetration and duration of fuel sprays from a pump injection system, by A.M. Rothrock and E.T. March [No. 455], p. 241 , Performance of a fuel-injection spark-ignition engine using a hydrogenated safety fuel, by Oscar W. Schey and Alfred W. Young [No. 471], p. 557 , Photomicrographic studies of fuel sprays, by Dana W. Lee and Robert C. Spencer [No. 454], p. 215 , Pressure-distribution measurements on the hull and fins of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 443], p. 67 , Relative loading on biplane wings, by Walter S. Diehl [No. 458], p. 275 , Static thrust of airplane propellers, by Walter S. Diehl [No. 447], p. 125 , Strength tests of thin-walled duralumin cylinders in compression, by Eugene E. Lundquist [No. 473], p. 585 , Tests of nacelle-propeller combinations in various positions with reference to wings. III. -- Clark Y wing -- Various radial-engine cowlings -- Tractor propeller, by Donald H. Wood [No. 462], p. 359 , The N.A.C.A. full-scale wind tunnel, by Smith J. De France [No. 459], p. 291 , The N.A.C.A. high-speed wind tunnel and tests of six propeller sections, by John Stack [No. 463], p. 399 , The N.A.C.A. tank: A high-speed towing basin for testing models of seaplane floats, by Starr Truscott [No. 470], p. 535 , The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance, by M.J. Bamber and C.H. Zimmerman [No. 456], p. 249 , The calculation of take-off run, by Walter S. Diehl [No. 450], p. 163 , The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel, by Eastman N. Jacobs, Kenneth E. Ward, and Robert M. Pinkerton [No. 460], p. 299 , The drag of two streamline bodies as affected by protuberances and appendages, by Ira H. Abbot [No. 451], p. 171 , The estimation of maximum load capacity of seaplanes and flying boats, by Walter S. Diehl [No. 453], p. 211 , The experimental determination of the moments of inertia of airplanes, by Hartley A. Soule and Marvel P. Miller [No. 467], p. 501 , The interference between struts in various combinations, by David Biermann and William H. Herrnstein, Jr. [No. 468], p. 515 , Wind-tunnel research comparing lateral control devices particularly at high angles of attack. VI. -- Skewed ailerons and rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 444], p. 81 , Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles, by Fred E. Weick and Robert Sanders [No. 472], p. 567 , Wing characteristics as affected by protuberances of short span, by Eastman N. Jacobs and Albert Sherman [No. 449], p. 155 , Working charts for the determination of the lift distribution between biplane wings, by Paul Kuhn [No. 445], p. 93 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
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  • 5
    UID:
    gbv_754046702
    Format: Online-Ressource (756 p) , illustrations, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 9667
    Note: A method for computing leading-edge loads, by Richard V. Rhode and Henry A. Pearson [No. 413], p. 249 , Aircraft speed instruments, by K. Hilding Beij [No. 420], p. 381 , Appendix, p. 237 , Application of practical hydrodynamics to airship design, by Ralph H. Upson and W.A. Klikoff [No. 405], p. 123 , Characteristics of Clark Y airfoils of small aspect ratios, by C.H. Zimmerman [No. 431], p. 581 , Combustion in a high-speed compression-ignited engine, by A.M. Rothrock [No. 401], p. 63 , Drop and flight tests on NY-2 landing gears including measurements of vertical velocities at landing, by W.C. Peck and A.P. Beard [No. 406], p. 141 , Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines, by A.G. Gelalles [No. 402], p. 79 , Experiments on the distribution of fuel in fuel sprays, by Dana W. Lee [No. 438], p. 703 , Force measurements on a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 432], p. 591 , Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 435], p. 629 , General formulas and charts for the calculation of airplane performance, by W. Bailey Oswald [No. 408], p. 163 , Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil, by Theodore Theodorsen and William C. Clay [No. 403], p. 91 , Lift and drag characteristics and gliding performance of an autogiro as determined in flight, by John B. Wheatley [No. 434], p. 621 , Measurement of the differential and total thrust and torque of six full-scale adjustable-pitch propellers, by George W. Stickle [No. 421], p. 437 , Measurements of flow in the boundary layer of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 430], p. 567 , Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics, by Fred E. Weick [No. 418], p. 343 , Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability, by Richard W. Noyes [No. 417], p. 315 , Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines, by A.G. Gelalles and E.T. Marsh [No. 433], p. 607 , Table of contents, p. VII , Tests of nacelle-propeller combinations in various positions with reference to wings. Part I. Thick wing -- N.A.C.A. cowled nacelle-tractor propeller, by Donald H. Wood [No. 415], p. 277 , Tests on nacelle-propeller combinations in various positions with reference to wings. II. -- Thick wing -- various radial-engine cowlings -- tractor propeller, by Donald H. Wood [No. 436], p. 653 , The 7 by 10 foot wind tunnel of the National Advisory Committee for Aeronautics, by Thomas A. Harris [No. 412], p. 241 , The N.A.C.A. apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests, by A.M. Rothrock [No. 429], p. 549 , The N.A.C.A. variable-density wind tunnel, by Eastman N. Jacobs and Ira H. Abbott [No. 416], p. 305 , The characteristics of a Clark Y wing model equipped with several forms of low-drag fixed slots, by Fred E. Weick and Carl J. Wenzinger [No. 407], p. 155 , The effect of area and aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages, by Hugh L. Dryden and B.H. Monish [No. 437], p. 693 , The effect of humidity on engine power at altitude, by D.B. Brooks and E.Z. Garlock [No. 426], p. 523 , The effect of increased carburetor pressure on engine performance at several compression ratios, by Oscar W. Schey and Vern G. Rollin [No. 404], p. 113 , The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil, by Fred E. Weick and Joseph A. Shortal [No. 427], p. 531 , The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays, by Dana W. Lee [No. 425], p. 505 , The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines, by William H. McAvoy, Oscar W. Schey, and Alfred W. Young [No. 414], p. 259 , The elimination of fire hazard due to back fires, by Theodore Theodorsen and Ira M. Freeman [No. 409], p. 211 , The mechanism of atomization accompanying solid injection, by R.A. Castleman, Jr. [No. 440], p. 735 , The theory of wind-tunnel wall interference, by Theodore Theodorsen [No. 410], p. 219 , Theory of wing sections of arbitrary shape, by Theodore Theodorsen [No. 411], p. 229 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. I. -- Ordinary ailerons on rectangular wings, by Fred E. Weick and Carl J. Wenzinger [No. 419], p. 357 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. II. -- Slotted ailerons and Frise ailerons, by Fred E. Weick and Richard W. Noyes [No. 422], p. 457 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. III. -- Ordinary ailerons rigged up 10 [degrees] when neutral, by Fred E. Weick and Carl J. Wenzinger [No. 423], p. 471 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. IV. -- Floating tip ailerons on rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 424], p. 481 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. V. -- Spoilers and ailerons on rectangular wings, Fred E. Weick and Joseph A. Shortal [No. 439], p. 719 , Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions, by Fred E. Weick and Millard J. Bamber [No. 428], p. 537 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
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  • 6
    UID:
    gbv_753895080
    Format: Online-Ressource (519 p) , illustrations, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 8873
    Note: Appendix, p. 218 , Table of contents, p. VI , Technical Report No. 257. Pressure distribution over a wing and tail rib of a VE-7 and of a TS airplane in flight, by J.W. Crowley, Jr., p. 77 , Technical Report No. 258. Some factors affecting the reproducibility of penetration and the cut-off of oil sprays for fuel injected engines, by E.G. Beardsley, p. 115 , Technical Report No. 259. Characteristics of propeller sections tested in the variable density wind tunnel, by Eastman N. Jacobs, p. 125 , Technical Report No. 260. The effect of a flap and ailerons on the N.A.C.A. M-6 airfoil section, by George J. Higgins and Eastman N. Jacobs, p. 141 , Technical Report No. 261. Resistance and cooling power of various radiators, by R.H. Smith, p. 161 , Technical Report No. 262. Friction of aviation engines, by S.W. Sparrow and M.A. Thorne, p. 177 , Technical Report No. 263. Preliminary flight tests of the N.A.C.A. Roots type aircraft engine supercharger, by Arthur W. Gardiner and Elliott G. Reid, p. 205 , Technical Report No. 264. Differential pressures on a pilot-venturi and a pilot-static nozzle over 360 degree pitch and yaw, by R.M. Bear, p. 221 , Technical Report No. 265. A full scale investigation of ground effect, by Elliott G. Reid, p. 231 , Technical Report No. 266. Air force and moment for N-20 wing with certain cut-outs, by R.H. Smith, p. 239 , Technical Report No. 267. Drag of wings with end plates, by Paul E. Henke, p. 251 , Technical Report No. 268. Factors in the design of centrifugal type injection valves for oil engines, by W.F. Joachim and E.G. Beardsley, p. 265 , Technical Report No. 269. Air force tests of Sperry Messenger model with six sets of wings, by James M. Shoemaker, p. 281 , Technical Report No. 270. The measurement of pressure through tubes in pressure distribution tests, by Paul E. Henke, p. 301 , Technical Report No. 271. Pressure distribution tests on PW-9 wing models, showing effects of biplane interference, by A.J. Fairbanks, p. 313 , Technical Report No. 272. The relative performance obtained with several methods of control of an overcompressed engine using gasoline, by Arthur W. Gardiner and William E. Whedon, p. 327 , Technical Report No. 273. Wind tunnel tests on autorotation and the "flat spin," by Montgomery Knight, p. 341 , Technical Report No. 274. The N.A.C.A. photographic apparatus for studying fuel sprays from oil injection valves and test results from several researches, by Edward G. Beardsley, p. 359 , Technical Report No. 275. The effect of the walls in closed type wind tunnels, by George J. Higgins, p. 373 , Technical Report No. 276. Combustion time in the engine cylinder and its effect on engine performance, by Charles F. Marvin, Jr., p. 391 , Technical Report No. 277. The comparative performance of an aviation engine at normal and high inlet air temperatures, by Arthur W. Gardiner and Oscar W. Schey, p. 407 , Technical Report No. 278. Lift, drag, and elevator hinge moments of Handley Page control surfaces, by R.H. Smith, p. 427 , Technical Report No. 279. Tests on models of three British airplanes in the variable density wind tunnel, by George J. Higgins and George L. DeFoe, p. 449 , Technical Report No. 280. The gaseous explosive reaction -- the effect of inert gases, by F.W. Stevens, p. 477 , Technical Report No. 281. The effects of fuel and cylinder gas densities on the characteristics of fuel sprays for oil engines, by W.F. Joachim and Edward G. Beardsley, p. 489 , Technical Report No. 282. The performance of several combustion chambers designed for aircraft oil engines, by William F. Joachim and Carlton Kemper, p. 499 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
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  • 7
    UID:
    gbv_75401424X
    Format: Online-Ressource (730 p) , illustrations, maps, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 9523
    Note: A method of flight measurement of spins, by Hartley A. Soule and Nathan F. Scudder [No. 377], p. 267 , A new chart for estimating the absolute ceiling of an airplane, by Walter S. Diehl [No. 368], p. 111 , A new principle of sound frequency analysis, by Theodore Theodorsen [No. 395], p. 605 , Aerodynamic characteristics of circular-arc airfoils at high speeds, by L.J. Briggs and H.L. Dryden [No. 365], p. 67 , Airship model tests in the variable density wind tunnel, by Ira H. Abbott [No. 394], p. 583 , Coefficients of discharge of fuel injection nozzles for compression-ignition engines, by A.G. Gelalles [ No. 373], p. 193 , Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections, by Hugh B. Freeman [No. 378], p. 283 , Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4 airplane, by William C. Peck [No. 366], p. 79 , Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch, by B.H. Monish [No. 370], p. 137 , Elastic instability of members having sections common in aircraft construction, by George W. Trayer and H.W. March [No. 382], p. 373 , Flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., and Robert D. Best [No. 399], p. 697 , Full-scale tests of metal propellers at high tip speeds, by Donald H. Wood [No. 375], p. 237 , Hydraulics of fuel injection pumps for compression-ignition engines, by A.M. Rothrock [No. 396], p. 621 , Investigation of damping liquids for aircraft instruments -- II, by M.R. Houseman and G.H. Keulegan [No. 398], p. 679 , Investigation of the diaphragm-type pressure cell, by Theodore Theodorsen [No. 388], p. 507 , Maneuverability investigation of an F6C-4 fighting airplane, by C.H. Dearborn and H.W. Kirschbaum [No. 386], p. 475 , Maneuverability investigation of the F6C-3 airplane with special flight instruments, by C.H. Dearborn and H.W. Kirschbaum [No. 369], p. 117 , On the theory of wing sections with particular reference to the lift distribution, by Theodore Theodorsen [No. 383], p. 411 , Present status of aircraft instruments, by Subcommittee on Instruments [No. 371], p. 153 , Pressure distribution over a thick, tapered and twisted monoplane wing model -- N.A.C.A. 81 J, by Carl J. Wenzinger [No. 367], p. 97 , Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight, by Richard V. Rhode and Eugene E. Lundquist [No. 380], p. 327 , Reduction of turbulence in wind tunnels, by Hugh L. Dryden [No. 392], p. 557 , Rolling moments due to rolling and yaw for four wing models in rotation, by Montgomery Knight and Carl J. Wenzinger [No. 379], p. 301 , Some approximate equations for the standard atmosphere, by Walter S. Diehl [No. 376], p. 257 , Span-load distribution as a factor in stability in roll, by Montgomery Knight and Richard W. Noyes [No. 393], p. 567 , Static, drop, and flight tests on Musselman type airwheels, by William C. Peck and Albert P. Beard [No. 381], p. 355 , Table of contents, p. VI , The aerodynamic characteristics of a slotted Clark Y wing as affected by the auxiliary airfoil position, by Carl J. Wenzinger and Joseph A. Shortal [No. 400], p. 707 , The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel, by Eastman N. Jacobs [No. 391], p. 545 , The automotive ignition coil, by T.H. Darnell [No. 374], p. 211 , The comparative performance of superchargers, by Oscar W. Schey [No. 384], p. 425 , The drag characteristics of several airships determined by deceleration tests, by F.J. Thompson and H.W. Kirschbaum [No. 397], p. 665 , The effect of small angles of yaw and pitch on the characteristics of airplane propellers, by Hugh B. Freeman [No. 389], p. 523 , The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level, by Oscar W. Schey and Arnold E. Biermann [No. 390], p. 533 , The gaseous explosive reaction -- the effect of pressure on the rate of propagation of the reaction zone and upon the rate of molecular transformation, by F.W. Stevens [No. 372], p. 175 , The vertical wind tunnel of the National Advisory Committee for Aeronautics, by Carl J. Wenzinger and Thomas A. Harris [No. 387], p. 499 , Wind tunnel tests on airfoil boundary layer control using a backward-opening slot, by Millard J. Bamber [No. 385], p. 439 , © 2007 by NewsBank, Inc. All rights reserved
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  • 8
    UID:
    gbv_753458098
    Format: Online-Ressource (20 p)
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 5611
    Note: © 2007 by NewsBank, Inc. All rights reserved
    Language: English
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  • 9
    UID:
    gbv_753991632
    Format: Online-Ressource (799 p) , illustrations, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 9348
    Note: A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291 , A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361 , Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539 , Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467 , Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451 , An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635 , An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573 , Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501 , Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145 , Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171 , Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607 , Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393 , Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121 , Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105 , Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419 , List of technical reports, p. VII , Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587 , Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669 , Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515 , Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319 , Table of contents, p. VI , Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557 , The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135 , The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219 , The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201 , The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83 , The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67 , The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685 , Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273 , Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
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    UID:
    gbv_753956381
    Format: Online-Ressource (787 p) , illustrations, tables
    Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
    Series Statement: United States congressional serial set serial set no. 9221
    Note: Table of contents, p. VI , Table of technical reports, p. VII , Technical Report No. 309. Joint report on standardization tests on N.P.L. R.A.F. 15 Airfoil Model, by Walter S. Diehl, p. 91 , Technical Report No. 310. Pressure element of constant logarithmic stiffness for temperature compensated altimeter, by W.G. Brombacher and F. Cordero, p. 111 , Technical Report No. 311. Aerodynamic theory and test of strut forms, by R.H. Smith, p. 125 , Technical Report No. 312. The prediction of airfoil characteristics, by George J. Higgins, p. 149 , Technical Report No. 313. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-I, by Fred E. Weick, p. 163 , Technical Report No. 314. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-II, by Fred E. Weick, p. 189 , Technical Report No. 315. Aerodynamic characteristics of airfoils-VI, by National Advisory Committee for Aeronautics, p. 211 , Technical Report No. 316. Tables for pressure of air coming to rest from various speeds, by A.F. Zahm and F.A. Louden, p. 247 , Technical Report No. 317. Wind tunnel tests on a series of wing models through a large angle of attack range. Part I -- Force tests, by Montgomery Knight and Carl J. Wenzinger, p. 255 , Technical Report No. 318. Speed and deceleration trials of U.S.S. Los Angeles, by S.J. DeFrance and C.P. Burgess, p. 305 , Technical Report No. 319. Aerodynamic characteristics of twenty-four air-foils at high speed, by L.J. Briggs and H.L. Dryden, p. 325 , Technical Report No. 320. The measurement of fluctuations of air speed by hot-wire anemometer, by H.L. Dryden and A.M. Kuethe, p. 357 , Technical Report No. 321. Fuel vapor pressures and the relation of vapor pressure to the preparation of fuel for combustion in fuel injection engines, by William F. Joachim and A.M. Rothrock, p. 383 , Technical Report No. 322. Investigation of air flow in open-throat wind tunnels, by Eastman N. Jacobs, p. 397 , Technical Report No. 323. Flow and force equations for a body revolving in fluid, by A.F. Zahm, p. 409 , Technical Report No. 324. Flight tests on U.S.S. Los Angeles. Part I. -- Full scale pressure distribution investigation, by S.J. DeFrance, p. 449 , Technical Report No. 325. Flight tests on U.S.S. Los Angeles. Part II. -- Stress and strength determination, by C.P. Burgess, p. 483 , Technical Report No. 326. Tests of five metal model propellers with various pitch distributions in a free wind stream and in combination with a model VE-7 fuselage, by E.P. Lesley and Elliott G. Reid, p. 499 , Technical Report No. 327. The effect of supercharger capacity on engine and airplane performance, by O.W. Schey and W.D. Gove, p. 517 , Technical Report No. 328. Water pressure distribution on a twin-float seaplane, by F.L. Thompson, p. 537 , Technical Report No. 329. The torsional strength of wings, by C.P. Burgess, p. 555 , Technical Report No. 330. Experimental and analytical determination of the motion of hydraulically operated valve stems in oil engine injection systems, by A.G. Gelalles and A.M. Rothrock, p. 569 , Technical Report No. 331. Collection of wind-tunnel data on commonly used wing sections, by F.A. Louden, p. 589 , Technical Report No. 332. The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine, by Oscar W. Schey and Arnold E. Biermann, p. 635 , Technical Report No. 333. Full-scale turning characteristics of the U.S.S. Los Angeles, by F.L. Thompson, p. 657 , Technical Report No. 334. The torsion of members having sections common in aircraft construction, by George W. Trayer and H.W. March, p. 671 , Technical Report No. 335. Aerodynamic theory and test of strut forms II, by R.H. Smith, p. 721 , Technical Report No. 336. Tests of large airfoils in the propeller research tunnel, including two with corrugated surfaces, by Donald H. Wood, p. 761 , © 2007 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
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