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Format: Online-Ressource (583 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. 10106

Note: A simplified application of the method of operators to the calculation of disturbed motions of an airplane, by Robert T. Jones [No. 560], p. 313 , Aerodynamic characteristics of N.A.C.A. 23012 and 23021 airfoils with 20-percent-chord external-airfoil flaps of N.A.C.A. 23012 section, by Robert C. Platt and Ira H. Abbott [No. 573], p. 523 , Air flow around finned cylinders, by M.J. Brevoort and Vern G. Rollin [No. 555], p. 237 , Air flow in the boundary layer near a plate, by Hugh L. Dryden [No. 562], p. 339 , Aircraft accidents method of analysis, report prepared by committee on aircraft accidents [No. 576], p. 564 , Aircraft compass characteristics, by John B. Peterson and Clyde W. Smith [No. 551], p. 187 , Calculated and measured pressure distributions over the midspan section of the N.A.C.A. 4412 airfoil, by Robert M. Pinkerton [No. 563], p. 365 , Combustion in a bomb with a fuel-injection system, by Mildred Cohn and Robert C. Spencer [No. 544], p. 107 , Cooling characteristics of a 2-row radial engine, by Oscar W. Schey and Vern G. Rollin [No. 550], p. 177 , Determination of the characteristics of tapered wings, by Raymond F. Anderson [No. 572], p. 503 , Effect of nozzle design on fuel spray and flame formation in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 561], p. 327 , Effect of tip shape and dihedral on lateral-stability characteristics, by Joseph A. Shortal [No. 548], p. 149 , Effects of air-fuel ratio on fuel spray and flame formation in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 545], p. 119 , Further studies of flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., Armistead Wharton, and Carl H. Roeder [No. 556], p. 251 , Ground-handling forces on a 1/40-scale model of the U.S. airship "Akron," by Abe Silverstein and B.G. Gulick [No. 566], p. 405 , Interference of wing and fuselage from tests of 28 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 575], p. 555 , List of technical reports, p. III , Measurements of fuel distribution within sprays for fuel-injection engines, by Dana W. Lee [No. 565], p. 389 , Potential flow about arbitrary biplane wing sections, by I.E. Garrick [No. 542], p. 47 , Preliminary tests in the N.A.C.A. free-spinning wind tunnel, by C.H. Zimmerman [No. 557], p. 265 , Pressure distribution over a rectangular airfoil with a partial-span split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 571], p. 491 , Pressure distribution over an airfoil section with a flap and tab, by Carl J. Wenzinger [No. 574], p. 543 , Propulsion of a flapping and oscillating airfoil, by I.E. Garrick [No. 567], p. 419 , Some effects of argon and helium upon explosions of carbon monoxide and oxygen, by Ernest F. Fiock and Carl H. Roeder [No. 553], p. 213 , Tank tests of N.A.C.A. model 40 series of hulls for small flying boats and amphibians, by John B. Parkinson and John R. Dawson [No. 543], p. 77 , Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ, by Ray Windler [No. 564], p. 381 , The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data, by Fred E. Weick and Robert T. Jones [No. 570], p. 465 , The effect of turbulence on the drag of flat plates, by G.B. Schubauer and H.L. Dryden [No. 546], p. 129 , The forces and moments acting on parts of the XN2Y-1 airplane during spins, by N.F. Scudder [No. 559], p. 305 , The quiescent-chamber type compression-ignition engine, by H.H. Foster [No. 568], p. 429 , Turbulence factors of N.A.C.A. wind tunnels as determined by sphere tests, by Robert C. Platt [No. 558], p. 283 , Wind-tunnel interference with particular reference to off-center positions of the wing and to the downwash at the tail, by Abe Silverstein and James A. White [No. 547], p. 135 , Wind-tunnel investigation of ordinary and split flaps on airfoils of different profile, by Carl J. Wenzinger [No. 554], p. 223 , Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps, by Carl J. Wenzinger [No. 549], p. 159 , Wind-tunnel tests of 10-foot-diameter auto-giro rotors, by John B. Wheatley and Carlton Bioletti [No. 552], p. 199 , Wing-nacelle-propeller interference for wings of various spans force and pressure-distribution tests, by Russel G. Robinson and William H. Herrnstein, Jr. [No. 569], p. 449 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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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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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

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (757 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10471

Note: A study of air flow in an engine cylinder, by Dana W. Lee [No. 653], p. 227 , A theoretical study of the moment on a body in a compressible fluid, by Karl Caplan [No. 671], p. 581 , Air flow in the boundary layer of an elliptic cylinder, by G.B. Schubauer [No. 652], p. 207 , Aircraft rate-of-climb indicators, by Daniel P. Johnson [No. 666], p. 473 , Airfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other corrections, by Eastman N. Jacobs and Ira H. Abbott [No. 669], p. 507 , Appendix, p. 69 , Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps, by Henry A. Pearson and Raymond F. Anderson [No. 665], p. 455 , Cooling on the front of an air-cooled engine cylinder in a conventional engine cowling, by M.J. Brevoort and U.T. Joyner [No. 674], p. 625 , Correction of temperatures of air-cooled engine cylinders for variation in engine and cooling conditions, by Oscar W. Schey, Benjamin Pinkel, and Herman H. Ellerbrock, Jr. [No. 645], p. 49 , Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings, by Abe Silverstein and S. Katzoff [No. 648], p. 107 , Design of N.A.C.A. cowlings for radial air-cooled engines, by George W. Stickle [No. 662], p. 383 , Determination of the profile drag of an airplane wing in flight at high Reynolds numbers, by Joseph Bicknell [No. 667], p. 483 , Downwash and wake behind plain and flapped airfoils, by Abe Silverstein, S. Katzoff, and W. Kenneth Bullivant [No. 651], p. 179 , Effect of service stresses on impact resistance, x-ray diffraction patterns and microstructure of 258 aluminum alloy, by J.A. Keyes and G.W. Quick [No. 659], p. 343 , Effects of elevator nose shape, gap, balance, and tabs, on the aerodynamic characteristics of a horizontal tail surface, by Harry J. Goett and J.P. Reeder [No. 675], p. 639 , Experimental investigation of the momentum method for determining profile drag, by Harry J. Goett [No. 660], p. 643 , Experimental verification of the theory of oscillating airfoils, by Abe Silverstein and Upshur T. Joyner [No. 673], p. 619 , Freen-spinning wind-tunnel tests in a low-wing monoplane with systematic changes in wings and tails -- IV. Effect of center-of-gravity location, by Oscar Seidman and A.I. Niehouse [No. 672], p. 599 , General airplane performance, by W.C. Rockefeller [No. 654], p. 241 , Interference with tail surface and wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 678], p. 689 , List of technical reports, p. III , Surface heat-transfer coefficients of finned cylinders, by Herman H. Ellerbrock, Jr. and Arnold E. Biermann [No. 676], p. 651 , Tensile elastic properties of 18:8 chromium-nickel steel as affected by plastic deformation, by D.J. McAdam, Jr. and R.W. Mebs [No. 670], p. 539 , Tests in the variable-density wind tunnel of the N.A.C.A. 23012 airfoil with plain and split flaps, by Ira H. Abbott and Harry Greenberg [No. 661], p. 373 , Tests of N.A.C.A. 0009, 0012, and 0018 airfoils in the full-scale tunnel, by Harry J. Goett and W. Kenneth Bullivant [No. 647], p. 97 , Tests of two full-scale propellers with different pitch distributions, at blade angles up to 60 degrees, by David Biermann and Edwin P. Hartman [No. 658], p. 327 , The "pack" method for compressive tests of thin specimens of materials used in thin-wall structures, by C.S. Aitchison and L.B. Tuckerman [No. 649], p. 133 , The aerodynamic characteristics of six full-scale propellers having different airfoil sections, by David Biermann and Edwin P. Hartman [No. 650], p. 145 , The column strength of two extruded aluminum-alloy h-sections, by William R. Osgood and Marshall Holt [No. 656], p. 289 , The compressibility burble and the effect of compressibility on pressures and forces acting on an airfoil, by John Stack, W.F. Lindsey, and Robert E. Littell [No. 646], p. 73 , The effect of Nacelle-propeller diameter ratio on body interference and on propeller and cooling characteristics, by James G. McHugh and Eldridge H. Derring [No. 680], p. 727 , The effect of continuous weathering of light metal alloys used in aircraft, by Willard Mutchler [No. 663], p. 395 , The influence of directed air flow on combustion in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 657], p. 313 , The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines, by A.M. Rothrock and Arnold E. Biermann [No. 655], p. 267 , Wind-tunnel investigation of N.A.C.A. 23012, 23021, 23030 airfoils with various sizes of split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 668], p. 493 , Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with a slotted flap and three types of auxiliary flap, by Carl J. Wenzinger and William E. Gauvain [No. 679], p. 699 , Wind-tunnel investigation of an N.A.C.A. 23021 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger and Thomas A. Harry [No. 677], p. 665 , Wind-tunnel investigation of an N.A.C.A. 23102 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger, and Thomas A. Harris [No. 664], p. 423 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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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

URL: Volltext  (Deutschlandweit zugänglich)