Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925

Media type: E-Book

Title: Aeronautics. Eleventh annual report of the National Advisory Committee for Aeronautics, 1925

Contributor: Ames, Joseph S. [Other]; Beardsley, Edward G. [Other]; Coolidge, Calvin [Other]; Crowley, John W. Jr [Other]; DeFrance, S.J. [Other]; Diehl, Walter S. [Other]; Dryden, Hugh Latimer [Other]; Durand, William Frederick [Other]; Heald, R.H. [Other]; Joachim, William F. [Other]; Lesley, E.P. [Other]; Louden, F.A. [Other]; Miller, Elton W. [Other]; Miller, Harold E. [Other]; Munk, Max M. [Other]; Reid, Elliott G. [Other]; Ronan, K.M. [Other]; Smith, R.H. [Other]; Sparrow, Stanwood W. [Other]; Zahm, Albert Francis [Other]; Taylor, D.W. [Other]; Tuckerman, L.B. [Other]; Ware, Marsden [Other]

Corporation: United States, President (1923-1929 : Coolidge) ; United States, National Advisory Committee for Aeronautics

imprint: Washington, DC, 1926
Online-Ausg.: Chester, Vt: NewsBank, inc, 2007

Extent: Online-Ressource (509 p); illustrations, tables

Language: English

Reproductino series: U.S. Congressional Serial Set, 1817-1980

Type of reproduction: Online-Ausg.

Place of reproduction: Chester, Vt: NewsBank, inc, 2007

Origination:

Footnote: A study of the effect of a diving start on airplane speed, by Walter S. Diehl, p. 421
Air forces, moments and damping on model of fleet airship Shenandoah, by A.F. Zahm, R.H. Smith, and F.A. Louden, p. 153
An investigation of the coefficient of discharge of liquids through small round orifices, by W.F. Joachim, p. 369
Characteristics of a boat type seaplane during take-off, by J.W. Crowley, Jr., and K.M. Ronan, p. 391
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
Description and laboratory tests of a Roots type aircraft engine supercharger, by Marsden Ware, p. 449
Fuels for high-compression engines, by Stanwood W. Sparrow, p. 481
Inertia factors of ellipsoids for use in airship design, by L.B. Tuckerman, p. 61
Investigation of turbulence in wind tunnels by a study of the flow about cylinders, by H.L. Dryden and R.H. Heald, p. 463
Model tests with a systematic series of 27 wing sections at full Reynolds number, by Max M. Munk and Elton W. Miller, p. 301
Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk, p. 203
Pressure distribution on the C-7 airship, by J.W. Crowley, Jr., and S.J. DeFrance, p. 327
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
Some aspects of the comparison of model and full-scale tests, by D.W. Taylor, p. 247
Spray penetration with a simple with a simple fuel injection nozzle, by Harold E. Miller and Edward G. Beardsley, p. 319
Stability equations for airship hulls, by A.F. Zahm, p. 83
Standard atmosphere--tables and data, by Walter S. Diehl, p. 219
Table of contents, p. VII
Table of technical reports, p. VIII
The air forces on a model of the Sperry Messenger airplane without propeller, by Max M. Munk and Walter S. Diehl, p. 379
The reduction of airplane flight test data to standard atmosphere conditions, by Walter S. Diehl and E.P. Lesley, p. 185
The variable density wind tunnel of the National Advisory Committee for Aeronautics, by Max M. Munk and Elton W. Miller, p. 403
Water model tests for semi-rigid airships, by L.B. Tuckerman, p. 69
Wing spar stress charts and wing truss proportions, by Edward P. Warner, p. 135
a resume of the advances in theoretical aeronautics made by Max M. Munk, by Joseph S. Ames, p. 89
© 2007 by NewsBank, Inc. All rights reserved

Search in field:

Recently searched for: