Aeronautics. Eighteenth annual report of the National Advisory Committee for Aeronautics, 1932. Including Technical Reports Nos. 401 to 440

Media type: E-Book

Title: Aeronautics. Eighteenth annual report of the National Advisory Committee for Aeronautics, 1932. Including Technical Reports Nos. 401 to 440

Contributor: Abbott, Ira H.A. [Other]; Bamber, Millard J. [Other]; Beard, Albert P. [Other]; Beij, K. Hilding [Other]; Brooks, Donal B. [Other]; Castleman, R.A. [Other]; Clay, William C. [Other]; Dryden, Hugh Latimer [Other]; Freeman, Hugh B. [Other]; Freeman, Ira Maximilian [Other]; Garlock, E.A. [Other]; Gelalles, A.G. [Other]; Harris, Thomas A. [Other]; Jacobs, Eastman N. [Other]; Klikoff, W.A. [Other]; Lee, Dana W. [Other]; Marsh, E.T. [Other]; McAvoy, William H. [Other]; Monish, B.H. [Other]; Rothrock, A.M. [Other]; Young, Alfred W. [Other]; Waldron, C.D. [Other]; Wenzinger, Carl Joseph [Other]; Zimmerman, Charles Horton [Other]; Wood, Donald H. [Other]; Weick, Fred E. [Other]; Stickle, George W. [Other]; Pearson, Henry A. [Other]; Wheatley, John B. [Other]; Shortal, Joseph Adams [Other]; Schey, Oscar W. [Other]; Upson, Ralph Hazlett [Other]; Rhode, Richard V. [Other]; Noyes, Richard W. [Other]; Theodorsen, Theodore [Other]; Rollin, Vern Gordon [Other]; Oswald, W. Bailey [Other]; Peck, William C. [Other]

Corporation: United States, National Advisory Committee for Aeronautics

Published: Washington, DC, 1933
Online-Ausg., Chester, Vt: NewsBank, inc, 2007

Extent: Online-Ressource (756 p); illustrations, tables

Language: English

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

Type of reproduction: Online-Ausg.

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

Origination:

Footnote: A method for computing leading-edge loads, by Richard V. Rhode and Henry A. Pearson [No. 413], p. 249
Aircraft speed instruments, by K. Hilding Beij [No. 420], p. 381
Appendix, p. 237
Application of practical hydrodynamics to airship design, by Ralph H. Upson and W.A. Klikoff [No. 405], p. 123
Characteristics of Clark Y airfoils of small aspect ratios, by C.H. Zimmerman [No. 431], p. 581
Combustion in a high-speed compression-ignited engine, by A.M. Rothrock [No. 401], p. 63
Drop and flight tests on NY-2 landing gears including measurements of vertical velocities at landing, by W.C. Peck and A.P. Beard [No. 406], p. 141
Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines, by A.G. Gelalles [No. 402], p. 79
Experiments on the distribution of fuel in fuel sprays, by Dana W. Lee [No. 438], p. 703
Force measurements on a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 432], p. 591
Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 435], p. 629
General formulas and charts for the calculation of airplane performance, by W. Bailey Oswald [No. 408], p. 163
Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil, by Theodore Theodorsen and William C. Clay [No. 403], p. 91
Lift and drag characteristics and gliding performance of an autogiro as determined in flight, by John B. Wheatley [No. 434], p. 621
Measurement of the differential and total thrust and torque of six full-scale adjustable-pitch propellers, by George W. Stickle [No. 421], p. 437
Measurements of flow in the boundary layer of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 430], p. 567
Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics, by Fred E. Weick [No. 418], p. 343
Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability, by Richard W. Noyes [No. 417], p. 315
Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines, by A.G. Gelalles and E.T. Marsh [No. 433], p. 607
Table of contents, p. VII
Tests of nacelle-propeller combinations in various positions with reference to wings. Part I. Thick wing -- N.A.C.A. cowled nacelle-tractor propeller, by Donald H. Wood [No. 415], p. 277
Tests on nacelle-propeller combinations in various positions with reference to wings. II. -- Thick wing -- various radial-engine cowlings -- tractor propeller, by Donald H. Wood [No. 436], p. 653
The 7 by 10 foot wind tunnel of the National Advisory Committee for Aeronautics, by Thomas A. Harris [No. 412], p. 241
The N.A.C.A. apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests, by A.M. Rothrock [No. 429], p. 549
The N.A.C.A. variable-density wind tunnel, by Eastman N. Jacobs and Ira H. Abbott [No. 416], p. 305
The characteristics of a Clark Y wing model equipped with several forms of low-drag fixed slots, by Fred E. Weick and Carl J. Wenzinger [No. 407], p. 155
The effect of area and aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages, by Hugh L. Dryden and B.H. Monish [No. 437], p. 693
The effect of humidity on engine power at altitude, by D.B. Brooks and E.Z. Garlock [No. 426], p. 523
The effect of increased carburetor pressure on engine performance at several compression ratios, by Oscar W. Schey and Vern G. Rollin [No. 404], p. 113
The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil, by Fred E. Weick and Joseph A. Shortal [No. 427], p. 531
The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays, by Dana W. Lee [No. 425], p. 505
The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines, by William H. McAvoy, Oscar W. Schey, and Alfred W. Young [No. 414], p. 259
The elimination of fire hazard due to back fires, by Theodore Theodorsen and Ira M. Freeman [No. 409], p. 211
The mechanism of atomization accompanying solid injection, by R.A. Castleman, Jr. [No. 440], p. 735
The theory of wind-tunnel wall interference, by Theodore Theodorsen [No. 410], p. 219
Theory of wing sections of arbitrary shape, by Theodore Theodorsen [No. 411], p. 229
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. I. -- Ordinary ailerons on rectangular wings, by Fred E. Weick and Carl J. Wenzinger [No. 419], p. 357
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. II. -- Slotted ailerons and Frise ailerons, by Fred E. Weick and Richard W. Noyes [No. 422], p. 457
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. III. -- Ordinary ailerons rigged up 10 [degrees] when neutral, by Fred E. Weick and Carl J. Wenzinger [No. 423], p. 471
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. IV. -- Floating tip ailerons on rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 424], p. 481
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. V. -- Spoilers and ailerons on rectangular wings, Fred E. Weick and Joseph A. Shortal [No. 439], p. 719
Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions, by Fred E. Weick and Millard J. Bamber [No. 428], p. 537
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