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Bear, R.M
[Sonstige Person, Familie und Körperschaft];
Beardsley, E.G
[Sonstige Person, Familie und Körperschaft];
Crowley, J.W
[Sonstige Person, Familie und Körperschaft];
DeFoe, George L.
[Sonstige Person, Familie und Körperschaft];
Fairbanks, A.J
[Sonstige Person, Familie und Körperschaft];
Gardiner, Arthur W.
[Sonstige Person, Familie und Körperschaft];
Hemke, Paul E.
[Sonstige Person, Familie und Körperschaft];
Higgins, George J.
[Sonstige Person, Familie und Körperschaft];
Jacobs, Eastman N.
[Sonstige Person, Familie und Körperschaft];
Joachim, William F.
[Sonstige Person, Familie und Körperschaft];
Kemper, Carlton
[Sonstige Person, Familie und Körperschaft];
Knight, Montgomery
[Sonstige Person, Familie und Körperschaft];
Marvin, Charles Frederick
[Sonstige Person, Familie und Körperschaft];
Reid, Elliott G.
[Sonstige Person, Familie und Körperschaft];
Schey, Oscar W.
[Sonstige Person, Familie und Körperschaft];
Shoemaker, James M.
[Sonstige Person, Familie und Körperschaft];
Smith, R.H
[Sonstige Person, Familie und Körperschaft];
Sparrow, Stanwood W.
[Sonstige Person, Familie und Körperschaft];
Stevens, F.W
[Sonstige Person, Familie und Körperschaft];
Thorne, M.A
[Sonstige Person, Familie und Körperschaft];
Whedon, William E.
[Sonstige Person, Familie und Körperschaft]
;
United States Congress Senate,
United States National Advisory Committee for Aeronautics
Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927
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- Medientyp: E-Book
- Titel: Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927
- Beteiligte: Bear, R.M. [Sonstige Person, Familie und Körperschaft]; Beardsley, E.G. [Sonstige Person, Familie und Körperschaft]; Crowley, J.W. [Sonstige Person, Familie und Körperschaft]; DeFoe, George L. [Sonstige Person, Familie und Körperschaft]; Fairbanks, A.J. [Sonstige Person, Familie und Körperschaft]; Gardiner, Arthur W. [Sonstige Person, Familie und Körperschaft]; Hemke, Paul E. [Sonstige Person, Familie und Körperschaft]; Higgins, George J. [Sonstige Person, Familie und Körperschaft]; Jacobs, Eastman N. [Sonstige Person, Familie und Körperschaft]; Joachim, William F. [Sonstige Person, Familie und Körperschaft]; Kemper, Carlton [Sonstige Person, Familie und Körperschaft]; Knight, Montgomery [Sonstige Person, Familie und Körperschaft]; Marvin, Charles Frederick [Sonstige Person, Familie und Körperschaft]; Reid, Elliott G. [Sonstige Person, Familie und Körperschaft]; Schey, Oscar W. [Sonstige Person, Familie und Körperschaft]; Shoemaker, James M. [Sonstige Person, Familie und Körperschaft]; Smith, R.H. [Sonstige Person, Familie und Körperschaft]; Sparrow, Stanwood W. [Sonstige Person, Familie und Körperschaft]; Stevens, F.W. [Sonstige Person, Familie und Körperschaft]; Thorne, M.A. [Sonstige Person, Familie und Körperschaft]; Whedon, William E. [Sonstige Person, Familie und Körperschaft]
- Körperschaft: United States, National Advisory Committee for Aeronautics
-
Erschienen:
Washington, DC, 1928
Online-Ausg.: Chester, Vt: NewsBank, inc, 2007 -
Erschienen in:
United States congressional serial set ; serial set no. 8873
Senate document / 70th Congress, 1st session. Senate ; no. 3 - Umfang: Online-Ressource (519 p); illustrations, tables
- Sprache: Englisch
- Reproduktionsreihe: U.S. Congressional Serial Set, 1817-1980
- Art der Reproduktion: Online-Ausg.
- Hersteller der Reproduktion: Chester, Vt: NewsBank, inc, 2007
- Entstehung:
-
Anmerkungen:
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
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