Coverart for item
The Resource Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364., (electronic resource)

Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364., (electronic resource)

Label
Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364.
Title
Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364.
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
1874-1964
http://library.link/vocab/relatedWorkOrContributorName
  • Anderson, Raymond F
  • Black, Goldie
  • Brombacher, W.G
  • Brueggeman, W.C
  • Davis, Merlin
  • Dryden, Hugh L.,
  • Durand, William Frederick
  • Foster, Hampton H
  • Harris, Thomas A
  • Heald, R.H
  • Hicks, Chester W
  • Hoover, Herbert
  • Jacobs, Eastman N
  • Joachim, William F
  • Knight, Montgomery
  • Kuethe, Arnold M.,
  • Markwardt, L.J
  • Melton, E.R
  • Millikan, Clark Blanchard
  • Monish, B.H
  • Newlin, J.A.,
  • Peters, Melville F
  • Pinkerton, Robert M
  • Rhode, Richard V
  • Rothrock, A.M
  • Schey, Oscar W
  • Schuman, Louis
  • Stack, John
  • Stevens, F.W
  • Strother, D.H
  • Summerville, Wayne L
  • Thompson, F.L
  • Trayer, George W.,
  • Weick, Fred E
  • Whittemore, H.L.,
  • Wood, Donald H
  • Young, Alfred W
  • United States
  • United States
Series statement
  • United States congressional serial set;
  • Senate document / 71st Congress, 3rd session. Senate
Series volume
  • serial set no. 9348
  • no. 219
http://library.link/vocab/subjectName
  • United States
  • Advisory boards, committees, etc
  • Aeronautics
  • Aircraft accidents and safety
  • Aircraft construction
  • Aircraft engines
  • Airplanes
  • Airships
  • Engineering
  • Internal combustion engines
  • Military aircraft
  • Technology
  • Transportation research
  • Transportation safety
  • Aircraft pilots
Label
Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364., (electronic resource)
Instantiates
Publication
Note
  • Table of contents, p. VI
  • List of technical reports, p. VII
  • The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67
  • The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83
  • Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105
  • Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121
  • The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135
  • Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145
  • Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171
  • The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201
  • The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219
  • Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273
  • A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291
  • Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319
  • A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361
  • Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377
  • Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393
  • Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419
  • Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451
  • Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467
  • Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501
  • Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515
  • Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539
  • Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557
  • An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573
  • Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587
  • Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607
  • An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635
  • Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669
  • The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685
Color
multicolored
Control code
NB00000222703
Dimensions
unknown
Extent
799 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)11C4D4BD84CE1E28
Terms governing use
©2007 by NewsBank, Inc. All rights reserved
Label
Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364., (electronic resource)
Publication
Note
  • Table of contents, p. VI
  • List of technical reports, p. VII
  • The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67
  • The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83
  • Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105
  • Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121
  • The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135
  • Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145
  • Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171
  • The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201
  • The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219
  • Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273
  • A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291
  • Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319
  • A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361
  • Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377
  • Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393
  • Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419
  • Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451
  • Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467
  • Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501
  • Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515
  • Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539
  • Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557
  • An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573
  • Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587
  • Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607
  • An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635
  • Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669
  • The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685
Color
multicolored
Control code
NB00000222703
Dimensions
unknown
Extent
799 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)11C4D4BD84CE1E28
Terms governing use
©2007 by NewsBank, Inc. All rights reserved

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