Kooperativer Bibliotheksverbund

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Format: Online-Ressource (509 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. 8560

Note: A study of the effect of a diving start on airplane speed, by Walter S. Diehl, p. 421 , Air forces, moments and damping on model of fleet airship Shenandoah, by A.F. Zahm, R.H. Smith, and F.A. Louden, p. 153 , An investigation of the coefficient of discharge of liquids through small round orifices, by W.F. Joachim, p. 369 , Characteristics of a boat type seaplane during take-off, by J.W. Crowley, Jr., and K.M. Ronan, p. 391 , Comparison of tests on air propellers in flight, with wind tunnel model tests on similar forms, by W.F. Durand and E. P. Lesley, p. 271 , Description and laboratory tests of a Roots type aircraft engine supercharger, by Marsden Ware, p. 449 , Fuels for high-compression engines, by Stanwood W. Sparrow, p. 481 , Inertia factors of ellipsoids for use in airship design, by L.B. Tuckerman, p. 61 , Investigation of turbulence in wind tunnels by a study of the flow about cylinders, by H.L. Dryden and R.H. Heald, p. 463 , Model tests with a systematic series of 27 wing sections at full Reynolds number, by Max M. Munk and Elton W. Miller, p. 301 , Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk, p. 203 , Pressure distribution on the C-7 airship, by J.W. Crowley, Jr., and S.J. DeFrance, p. 327 , Pressure distribution over thick tapered airfoils, N.A.C.A. 81, U.S.A. 27 C Modified and U.S.A. 35, by Elliott G. Reid, p. 431 , Some aspects of the comparison of model and full-scale tests, by D.W. Taylor, p. 247 , Spray penetration with a simple with a simple fuel injection nozzle, by Harold E. Miller and Edward G. Beardsley, p. 319 , Stability equations for airship hulls, by A.F. Zahm, p. 83 , Standard atmosphere--tables and data, by Walter S. Diehl, p. 219 , Table of contents, p. VII , Table of technical reports, p. VIII , The air forces on a model of the Sperry Messenger airplane without propeller, by Max M. Munk and Walter S. Diehl, p. 379 , The reduction of airplane flight test data to standard atmosphere conditions, by Walter S. Diehl and E.P. Lesley, p. 185 , The variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk and Elton W. Miller, p. 403 , Water model tests for semi-rigid airships, by L.B. Tuckerman, p. 69 , Wing spar stress charts and wing truss proportions, by Edward P. Warner, p. 135 , a resume of the advances in theoretical aeronautics made by Max M. Munk, by Joseph S. Ames, p. 89 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

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UID:

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)

UID:

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

URL: Volltext  (Deutschlandweit zugänglich)

UID:

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

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