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The Resource Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925., (electronic resource)

Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925., (electronic resource)

Label
Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925.
Title
Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925.
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/relatedWorkOrContributorDate
1872-1933
http://library.link/vocab/relatedWorkOrContributorName
  • Ames, Joseph S
  • Beardsley, Edward G
  • Coolidge, Calvin
  • Crowley, John W. Jr
  • DeFrance, S.J
  • Diehl, Walter S
  • Dryden, Hugh L.,
  • Durand, William Frederick
  • Heald, R.H
  • Joachim, William F
  • Lesley, E.P
  • Louden, F.A
  • Miller, Elton W
  • Miller, Harold E
  • Munk, Max M
  • Reid, Elliott G
  • Ronan, K.M
  • Smith, R.H
  • Sparrow, Stanwood W
  • Taylor, D.W
  • Tuckerman, L.B
  • Ware, Marsden
  • Warner, Edward P
  • Zahm, Albert Francis
  • United States
  • United States
Series statement
  • United States congressional serial set;
  • Senate document / 69th Congress, 1st session. Senate
Series volume
  • serial set no. 8560
  • no. 17
http://library.link/vocab/subjectName
  • United States
  • Aeronautics
  • Aircraft accidents and safety
  • Aircraft engines
  • Airplanes
  • Airships
  • Engineering
  • Military aircraft
  • Technology
  • Transportation research
  • Transportation safety
  • Standards
Label
Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925., (electronic resource)
Instantiates
Publication
Note
  • Table of contents, p. VII
  • Table of technical reports, p. VIII
  • Inertia factors of ellipsoids for use in airship design, by L.B. Tuckerman, p. 61
  • Water model tests for semi-rigid airships, by L.B. Tuckerman, p. 69
  • Stability equations for airship hulls, by A.F. Zahm, p. 83
  • a resume of the advances in theoretical aeronautics made by Max M. Munk, by Joseph S. Ames, p. 89
  • Wing spar stress charts and wing truss proportions, by Edward P. Warner, p. 135
  • Air forces, moments and damping on model of fleet airship Shenandoah, by A.F. Zahm, R.H. Smith, and F.A. Louden, p. 153
  • The reduction of airplane flight test data to standard atmosphere conditions, by Walter S. Diehl and E.P. Lesley, p. 185
  • Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk, p. 203
  • Standard atmosphere--tables and data, by Walter S. Diehl, p. 219
  • Some aspects of the comparison of model and full-scale tests, by D.W. Taylor, p. 247
  • 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
  • Model tests with a systematic series of 27 wing sections at full Reynolds number, by Max M. Munk and Elton W. Miller, p. 301
  • Spray penetration with a simple with a simple fuel injection nozzle, by Harold E. Miller and Edward G. Beardsley, p. 319
  • Pressure distribution on the C-7 airship, by J.W. Crowley, Jr., and S.J. DeFrance, p. 327
  • An investigation of the coefficient of discharge of liquids through small round orifices, by W.F. Joachim, p. 369
  • The air forces on a model of the Sperry Messenger airplane without propeller, by Max M. Munk and Walter S. Diehl, p. 379
  • Characteristics of a boat type seaplane during take-off, by J.W. Crowley, Jr., and K.M. Ronan, p. 391
  • The variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk and Elton W. Miller, p. 403
  • A study of the effect of a diving start on airplane speed, by Walter S. Diehl, p. 421
  • 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
  • Description and laboratory tests of a Roots type aircraft engine supercharger, by Marsden Ware, p. 449
  • Investigation of turbulence in wind tunnels by a study of the flow about cylinders, by H.L. Dryden and R.H. Heald, p. 463
  • Fuels for high-compression engines, by Stanwood W. Sparrow, p. 481
Color
multicolored
Control code
NB00000207719
Dimensions
unknown
Extent
509 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)11AB856E5D9380B0
Terms governing use
©2007 by NewsBank, Inc. All rights reserved
Label
Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925., (electronic resource)
Publication
Note
  • Table of contents, p. VII
  • Table of technical reports, p. VIII
  • Inertia factors of ellipsoids for use in airship design, by L.B. Tuckerman, p. 61
  • Water model tests for semi-rigid airships, by L.B. Tuckerman, p. 69
  • Stability equations for airship hulls, by A.F. Zahm, p. 83
  • a resume of the advances in theoretical aeronautics made by Max M. Munk, by Joseph S. Ames, p. 89
  • Wing spar stress charts and wing truss proportions, by Edward P. Warner, p. 135
  • Air forces, moments and damping on model of fleet airship Shenandoah, by A.F. Zahm, R.H. Smith, and F.A. Louden, p. 153
  • The reduction of airplane flight test data to standard atmosphere conditions, by Walter S. Diehl and E.P. Lesley, p. 185
  • Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk, p. 203
  • Standard atmosphere--tables and data, by Walter S. Diehl, p. 219
  • Some aspects of the comparison of model and full-scale tests, by D.W. Taylor, p. 247
  • 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
  • Model tests with a systematic series of 27 wing sections at full Reynolds number, by Max M. Munk and Elton W. Miller, p. 301
  • Spray penetration with a simple with a simple fuel injection nozzle, by Harold E. Miller and Edward G. Beardsley, p. 319
  • Pressure distribution on the C-7 airship, by J.W. Crowley, Jr., and S.J. DeFrance, p. 327
  • An investigation of the coefficient of discharge of liquids through small round orifices, by W.F. Joachim, p. 369
  • The air forces on a model of the Sperry Messenger airplane without propeller, by Max M. Munk and Walter S. Diehl, p. 379
  • Characteristics of a boat type seaplane during take-off, by J.W. Crowley, Jr., and K.M. Ronan, p. 391
  • The variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk and Elton W. Miller, p. 403
  • A study of the effect of a diving start on airplane speed, by Walter S. Diehl, p. 421
  • 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
  • Description and laboratory tests of a Roots type aircraft engine supercharger, by Marsden Ware, p. 449
  • Investigation of turbulence in wind tunnels by a study of the flow about cylinders, by H.L. Dryden and R.H. Heald, p. 463
  • Fuels for high-compression engines, by Stanwood W. Sparrow, p. 481
Color
multicolored
Control code
NB00000207719
Dimensions
unknown
Extent
509 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)11AB856E5D9380B0
Terms governing use
©2007 by NewsBank, Inc. All rights reserved

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