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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

URL: Volltext  (Deutschlandweit zugänglich)

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Format: 1 online resource (4 pages, 3 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 240

Note: "June 1926." , No Federal Depository Library Program (FDLP) item number.

Language: English

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Format: 1 online resource (6 pages, 1 unnumbered page) : , illustration.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 243

Note: "August 1926." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (4 pages, 3 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 240

Note: "June 1926." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (6 pages, 1 unnumbered page) : , illustration.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 243

Note: "August 1926." , No Federal Depository Library Program (FDLP) item number.

Language: English

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Format: 1 online resource (13 pages, 30 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 219

Note: "May 1925." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (13 pages, 30 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 219

Note: "May 1925." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (6 pages, 10 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 256

Note: "March 1927." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (10 pages, 9 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 295

Note: "August 1928." , "Based on a Thesis present by Dronin and Ramsden for the B.S. degree in Engineering at New York University"--Page 1. , No Federal Depository Library Program (FDLP) item number.

Language: English