Report. Aeronautics, 13th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1927 [including Technical reports 257-282].
Publication Title:
Report. Aeronautics, 13th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1927 [including Technical reports 257-282].
Display Title:
Report. Aeronautics, 13th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1927 [including Technical reports 257-282].
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1928
Publish Date ISO Format:
1928-01-01T00:00:00Z
Publication Start:
19280101
Publication End:
19281231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1928
SuDoc number:
Y 3.N 21/5:1/927-2
Description:
viii+510 p. il. 1 por. 1 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, $1.25.
Notes:
CONTENTS.—13th annual report.—Report 257. Pressure distribution over wing and tail rib of VE-7 and of TS airplane in flight [with list of references]; by J. W. Crowley, jr.—Report 258. Some factors affecting reproducibility of penetration and cut-off of oil sprays for fuel-injection engines [with references and bibliography]; by E. G. Beardsley.—Report 259. Characteristics of propeller sections tested in variable density wind tunnel [with list of references]; by Eastman N. Jacobs.—Report 260. Effect of flap and ailerons on N. A. C. A. M-6 airfoil section [with list of references]; by George J. Higgins and Eastman N. Jacobs.—Report 261. Resistance and cooling power of various radiators [with list of references]; by R. H. Smith.—Report 262. Friction of aviation engines [with bibliography]; by S. W. Sparrow and M. A. Thome.—Report 263. Preliminary flight tests of N. A. C. A. Roots type aircraft engine supercharger [with bibliography]; by Arthur W. Gardiner and Elliott G. Reid.—Report 264. Differential pressures on pilot-venturi and pilot-static nozzle over 360° pitch and yaw [with list of references]; by R. M. Bear.—Report 265. Full-scale investigation of ground effect [with references and bibliography]; by Elliott G. Reid.—Report 266. Air force and moment for N-20 wing with certain cut-outs [with reference]; by R. H. Smith.—Report 267. Drag of wings with end plates [with list of references]; by Paul E. Hemke.—Report 268. Factors in design of centrifugal type injection valves for oil engines [with list of references]; by W. F. Joachim and E. G. Beardsley.—Report 269. Air force tests of Sperry Messenger model with 6 sets of wings [with list of references]; by James M. Shoemaker.—Report 270. Measurement of pressure through tubes in pressure distribution tests [with list of references]; by Paul E. Hemke.—Report 271. Pressure distribution tests on PW-9 wing models snowing effects of biplane interference [with references and bibliography]; by A. J. Fairbanks.—Report 272. Relative performance obtained with several methods of control of overcompressed engine using gasoline [with references and bibliography]; by Arthur W. Gardiner and William E. Whedon.—Report 273. Wind tunnel tests on autorotation and flat spin [with references and bibliography]; by Montgomery Knight.—Report 274. N. A. C. A. photographic apparatus for studying fuel sprays from oil engine injection valves and test results from several researches [with reference]; by Edward G. Beardsley.—Report 275. Effect of walls in closed type wind tunnels [with list of references]; by George J. Higgins.—Report 276. Combustion time in engine cylinder and its effect on engine performance [with reference]; by Charles F. Marvin, jr.—Report 277. Comparative performance of aviation engine at normal and high inlet air temperatures [with list of references]; by Arthur W. Gardiner and Oscar W. Schey.—Report 278. Lift, drag, and elevator hinge moments of Handley Page control surfaces [with reference]; by R. H. Smith.—Report 279. Tests on models of 3 British airplanes in variable density wind tunnel [with list of references], by George J. Higgins, George L. DeFoe, [and] W. S. Diehl; [and with Report of Aerodynamics Subcommittee, British Aeronautical Research Committee: Tests of 3 airplane models, by H. C. H. Townend].—Report 280. Gaseous explosive reaction, effect of inert gases [with list of references]; by F. W. Stevens.—Report 281. Effects of fuel and cylinder gas densities on characteristics of fuel sprays for oil engines [with list of references]; by W. F. Joachim and Edward G. Beardsley.—Report 282. Performance of several combustion chambers designed for aircraft oil engines [with list of references]; by William F. Joachim and Carlton Kemper.
Availability:
* For Sale by Superintendent of Documents. Paper, $1.25.