Coverart for item
The Resource Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927., (electronic resource)

Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927., (electronic resource)

Label
Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927.
Title
Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927.
Creator
Contributor
Subject
Genre
Language
eng
Member of
Cataloging source
Readex
Government publication
federal national government publication
Index
no index present
Literary form
non fiction
Nature of contents
dictionaries
http://bibfra.me/vocab/lite/organizationName
United States
http://library.link/vocab/relatedWorkOrContributorName
  • Bear, R.M
  • Beardsley, E.G
  • Crowley, J.W.
  • DeFoe, George L
  • Fairbanks, A.J
  • Gardiner, Arthur W
  • Hemke, Paul E
  • Higgins, George J
  • Jacobs, Eastman N
  • Joachim, William F
  • Kemper, Carlton
  • Knight, Montgomery
  • Marvin, Charles F.,
  • Reid, Elliott G
  • Schey, Oscar W
  • Shoemaker, James M
  • Smith, R.H
  • Sparrow, Stanwood W
  • Stevens, F.W
  • Thorne, M.A
  • Whedon, William E
  • United States
Series statement
  • United States congressional serial set;
  • Senate document / 70th Congress, 1st session. Senate
Series volume
  • serial set no. 8873
  • no. 3
http://library.link/vocab/subjectName
  • United States
  • Advisory boards, committees, etc
  • Aeronautics
  • Aircraft engines
  • Airplanes
  • Airships
  • Military aircraft
  • Transportation research
Label
Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927., (electronic resource)
Instantiates
Publication
Note
  • 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
  • Appendix, p. 218
Color
multicolored
Control code
NB00000212957
Dimensions
unknown
Extent
519 p.
Form of item
electronic
Governing access note
Access restricted to subscribing institutions
Other physical details
illustrations, tables
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
(Readex)11B7A8D6D5571E98
Terms governing use
©2007 by NewsBank, Inc. All rights reserved
Label
Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927., (electronic resource)
Publication
Note
  • 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
  • Appendix, p. 218
Color
multicolored
Control code
NB00000212957
Dimensions
unknown
Extent
519 p.
Form of item
electronic
Governing access note
Access restricted to subscribing institutions
Other physical details
illustrations, tables
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
(Readex)11B7A8D6D5571E98
Terms governing use
©2007 by NewsBank, Inc. All rights reserved

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