Coverart for item
The Resource Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308., (electronic resource)

Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308., (electronic resource)

Label
Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308.
Title
Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308.
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
  • Crowley, J.W.
  • Diehl, Walter S
  • Gove, W.D
  • Green, M.W
  • Heald, R.H
  • Hicks, Chester W
  • Keulegan, Garbis H.,
  • Knight, Montgomery
  • Loeser, Oscar E.
  • Louden, F.A
  • Mixson, R.E
  • Rhode, Richard V
  • Schey, Oscar W
  • Smith, R.H
  • Stevens, F.W
  • Strother, D.H
  • Ware, Marsden
  • Weick, Fred E
  • Wilson, Ernest E
  • Wood, Donald H
  • Zahm, Albert Francis
  • United States
Series statement
  • United States congressional serial set;
  • Senate document / 70th Congress, 2nd session. Senate
Series volume
  • serial set no. 9003
  • no. 178
http://library.link/vocab/subjectName
  • United States
  • Aeronautics
  • Aircraft accidents and safety
  • Aircraft engines
  • Airplanes
  • Engineering
  • Military aircraft
  • Transportation research
  • Aircraft pilots
  • Research
Label
Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308., (electronic resource)
Instantiates
Publication
Note
  • Table of contents, p. VI
  • A preliminary investigation of supercharging an air-cooled engine in flight, by Marsden Ware and Oscar W. Schey [No. 283], p. 81
  • The comparative performance of roots type aircraft engine superchargers as affected by change in impeller speed and displacement, by Marsden Ware and Ernest E. Wilson [No. 284], p. 93
  • A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107
  • Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135
  • Theories of flow similitude, by A.F. Zahm [No. 287], p. 185
  • Pressure distribution over a rectangular monoplane wing model up to 90' angle of attack, by Montgomery Knight and Ocsar Loeser, Jr. [No. 288], p. 195
  • Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215
  • Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233
  • Drag of C-class airship hulls of various fineness ratios, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 291], p. 249
  • Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265
  • Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane, by Walter S. Diehl [No. 293], p. 289
  • The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309
  • The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321
  • Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333
  • Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355
  • Effect of variation of chord and span of ailerons on rolling and yawing moments in level flight, by R.H. Heald and D.H. Strother [No. 298], p. 383
  • Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403
  • The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics, by Fred E. Weick and Donald H. Wood [No. 300], p. 427
  • Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463
  • An investigation of the use of discharge valves and intake control for improving the performance of N.A.C.A. Roots Type Supercharger, by Oscar W. Schey and Ernest E. Wilson [No. 302], p. 477
  • An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 303], p. 477
  • An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 304], p. 487
  • The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501
  • Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519
  • The pressure distribution over the horizontal and vertical tail surfaces of the F6C-4 pursuit airplane in violent maneuvers, by R.V. Rhode [No. 307], p. 537
  • Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557
Color
multicolored
Control code
NB00000216840
Dimensions
unknown
Extent
582 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)11B9EFC76866AE90
Terms governing use
©2007 by NewsBank, Inc. All rights reserved
Label
Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308., (electronic resource)
Publication
Note
  • Table of contents, p. VI
  • A preliminary investigation of supercharging an air-cooled engine in flight, by Marsden Ware and Oscar W. Schey [No. 283], p. 81
  • The comparative performance of roots type aircraft engine superchargers as affected by change in impeller speed and displacement, by Marsden Ware and Ernest E. Wilson [No. 284], p. 93
  • A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107
  • Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135
  • Theories of flow similitude, by A.F. Zahm [No. 287], p. 185
  • Pressure distribution over a rectangular monoplane wing model up to 90' angle of attack, by Montgomery Knight and Ocsar Loeser, Jr. [No. 288], p. 195
  • Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215
  • Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233
  • Drag of C-class airship hulls of various fineness ratios, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 291], p. 249
  • Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265
  • Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane, by Walter S. Diehl [No. 293], p. 289
  • The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309
  • The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321
  • Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333
  • Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355
  • Effect of variation of chord and span of ailerons on rolling and yawing moments in level flight, by R.H. Heald and D.H. Strother [No. 298], p. 383
  • Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403
  • The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics, by Fred E. Weick and Donald H. Wood [No. 300], p. 427
  • Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463
  • An investigation of the use of discharge valves and intake control for improving the performance of N.A.C.A. Roots Type Supercharger, by Oscar W. Schey and Ernest E. Wilson [No. 302], p. 477
  • An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 303], p. 477
  • An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 304], p. 487
  • The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501
  • Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519
  • The pressure distribution over the horizontal and vertical tail surfaces of the F6C-4 pursuit airplane in violent maneuvers, by R.V. Rhode [No. 307], p. 537
  • Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557
Color
multicolored
Control code
NB00000216840
Dimensions
unknown
Extent
582 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)11B9EFC76866AE90
Terms governing use
©2007 by NewsBank, Inc. All rights reserved

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