Report. Aeronautics, 11th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1925, including Technical reports 210-232.
Publication Title:
Report. Aeronautics, 11th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1925, including Technical reports 210-232.
Display Title:
Report. Aeronautics, 11th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1925, including Technical reports 210-232.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1926
Publish Date ISO Format:
1926-01-01T00:00:00Z
Publication Start:
19260101
Publication End:
19261231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1926
SuDoc number:
Y 3.N 21/5:1/925-2
Description:
ix+500 p. il. 4 p. of pl. 4°
Notes:
[Each report is also published separately in advance.]
Notes:
[Each report is also published separately in advance.] * For Sale by Superintendent of Documents. Paper, $1.00.
Notes:
CONTENTS.—11th annual report.—Report 210. Inertia factors of ellipsoids for use in airship design; by L. B. Tuckerman.—Report 211. Water model tests for semirigid airships; by L. B. Tuckerman.—Report 212. Stability equations for airship hulls; by A. F. Zahm.—Report 213. Résumé of advances in theoretical aeronautics made by Max M. Munk [with lists of references]; by Joseph S. Ames.—Report 214. Wing spar stress charts and wing truss proportions; by Edward P. Warner.—Report 215. Air forces, moments, and damping on model of fleet airship Shenandoah; by A. F. Zahm, R. H. Smith, and F. A. Louden.—Report 216. Reduction of airplane flight test data to standard atmosphere conditions: [pt. 1, Reduction of test data in climb to standard conditions, simple approximate method, by Walter S. Diehl; pt. 2. Reduction of airplane performance in climb to standard conditions, by E. P. Lesley; pt. 3, Conversion of air-speed indicator readings into true air speeds, air-speed indicator, by Walter S. Diehl].—Report 217. Preliminary wing model tests in variable density wind tunnel of National Advisory Committee for Aeronautics [with list of references], by Max M. Munk; [with Comparison with theory, by George J. Higgins].—Report 218. Standard atmosphere, tables and data [with list of references]; by Walter S. Diehl.—Report 219. Some aspects of comparison of model and full-scale tests; by D. W. Taylor.— Report 220. Comparison of tests on air propellers in flight with wind tunnel model tests on similar forms [with reference]; by W. F. Durand and E. P. Lesley.—Report 221. Model tests with systematic series of 27 wing sections at full Reynolds number; by Max M. Munk and Elton W. Miller.—Report 222. Spray penetration with simple fuel injection nozzle [with reference]; by Harold E. Miller and Edward G. Beardsley.— Report 223. Pressure distribution on C-7 airship [with bibliography]; by J. W. Crowley. jr., and S. J. DeFrance.—Report 224. Investigation of coefficient of discharge of liquids through small round orifices; by W. F. Joachim.—Report 225. Air forces on model of Sperry Messenger airplane without propeller [with bibliography]; by Max M. Munk and Walter S. Diehl.—Report 226. Characteristics of boat type seaplane during take-off [with bibliography]; by J. W. Crowley, jr., and K. M. Ronan.—Report 227. Variable density wind tunnel of National Advisory Committee for Aeronautics [with list of references: pt. 1, Fundamental principles, by Max M. Munk; pt. 2, Description of tunnel, by Elton W. Miller].—Report 228. Study of effect of diving start on airplane speed; by Walter S. Diehl.—Report 229. Pressure distribution over thick tapered airfoils, N. A. C. A. 81. U. S. A. 27 C modified, and U. S. A. 35 [with list of references]; by Elliott G. Reid.—Report 230. Description and laboratory tests of Roots type aircraft engine supercharger; by Marsden Ware.—Report 231. Investigation of turbulence in wind tunnels by study of flow about cylinders [with bibliography and references]; by H. L. Dryden and R. H. Heald.—Report 232. Fuels for high-compression engines [with bibliography]; by Stanwood W. Sparrow.
Availability:
* For Sale by Superintendent of Documents. Paper, $1.00.