Report. Aeronautics, 18th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1932, including Technical reports 401-440.
Publication Title:
Report. Aeronautics, 18th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1932, including Technical reports 401-440.
Display Title:
Report. Aeronautics, 18th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1932, including Technical reports 401-440.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1933
Publish Date ISO Format:
1933-01-01T00:00:00Z
Publication Start:
19330101
Publication End:
19331231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1933
SuDoc number:
Y 3.N 21/5:1/932-2
Description:
x+746 p. il. 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. Cloth, $2.50.
Notes:
CONTENTS.—18th annual report.—Report 401. Combustion in high-speed compression-ignition engine [with list of references]; by A. M. Rothrock.—Report 402. Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines [with list of references]; by A. G. Gelalles.—Report 403. Ice prevention on aircraft by means of engine exhaust beat and technical study of beat transmission from Clark Y airfoil [with list of references]; by Theodore Theodorsen and William C. Clay.—Report 404. Effect of Increased carburetor pressure on engine performance at several compression ratios [with references and bibliography]; by Oscar W. Schey and Vern G. Rollin.—Report 405. Application of practical hydrodynamics to airship design [with list of references]; by Ralph H. Upson and W. A. Klikoff.—Report 406. Drop and flight tests on NY-2 landing gears, including measurements of vertical velocities at landing [with list of references]; by W. C. Peck and A. P. Beard.—Report 407. Characteristics of Clark Y wing model equipped with several forms of low-drag fixed slots [with list of references]; by Fred E. Weick and Carl J. Wenzlnger.—Report 408. General formulas and charts for calculation of airplane performance [with list of references]; by W. Bailey Oswald.—Report 409. Elimination of fire hazard due to back fires [with list of references]: by Theodore Theodorsen and Ira M. Freeman.—Report 410. Theory of wind-tunnel wall interference [with list of references]: by Theodore Theodorsen.— Report 411. Theory of wing sections of arbitrary shape [with list of references]; by Theodore Theodorsen.—Report 412. The 7 by 10 foot wind tunnel of National Advisory Committee for Aeronautics [with list of references]; by Thomas A. Harris.—Report 413. Method for computing leading-edge loads [with list of references!; by Richard V. Rhode and Henry A. Pearson.—Report 414. Effect on airplane performance of factors that must be considered in applying low-drag cowling to radial engines [with list of references]; by William H. McAvoy, Oscar W. Schey, and Alfred W. Young.—Report 415. Tests of nacelle-propeller combinations in various positions with reference to wings: pt. 1, Thick wing, N. A. C. A. cowled nacelle, tractor propeller [with list of references]; by Donald H. Wood.—Report 416. N. A. C. A. variabledensity wind tunnel (with list of references]; by Eastman N. Jacobs and Ira H. Abbott.—Report 417. Pressure distribution tests on series of Clark Y biplane cellules with special reference to stability [with list of references]; by Richard W. Noyes.— Report 418. Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics [with list of references]: by Fred E. Weick.—Report 419. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack: 1. Ordinary ailerons on rectangular wings [with list of references]; by Fred E. Weick and Carl J. Wenzinger.—Report 420. Aircraft speed instruments [with list of references]; by K. Hilding Beij.—Report 421. Measurement of differential and total thrust and torque of 6 full-scale adjustable-pitch propellers [with list of references]; by George W. Stickle.—Report 422. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack: 2. Slotted ailerons and Frise ailerons [with list of references]; by Fred E. Weick and Richard W. Noyes.—Report 423. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack: 3, Ordinary ailerons rigged up 10° when neutral [with list of references]; by Fred E. Weick and Carl 3. Wenzinger.—Report 424. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack: 4. Floating tip ailerons on rectangular wings [with list of references]; by Fred E. Weick and Thomas A. Harris.—Report 425. Effect of nozzle design and operating conditions on atomization and distribution of fuel sprays f with references and bibliography]: by Dana W. Lee.—Report 426. Effect of humidity on engine power at altitude [with bibliography]; by D. B. Brooks and E. A. Garlock.—Report 427. Effect of multiple fixed slots and trailing-edge flap on lift and drag of Clark Y airfoil [with list of references]; by Fred E. Weick and Joseph A. Shortal.—Report 428. Wind-tunnel tests of Clark Y wing with narrow auxiliary airfoil in different positions [with references and bibliography]; by Fred E. Weick and Millard J. Bamber.—Report 429. N. A. C. A. apparatus for studying formation and combustion of fuel sprays and results from preliminary tests [with list of references]; by A. M. Rothrock.—Report 430. Measurements of flow in boundary layer of 1/40-scale model of U.S. airship Akron [with list of references]; by Hugh B. Freeman.—Report 431. Characteristics of Clark Y airfoils of small aspect ratios [with list of references]: by C. H. Zimmerman.—Report 432. Force measurements on 1/40-scale model of U.S. airship Akron [with list of references]: by Hugh B. Freeman.—Report 433. Rates of fuel discharge as affected by design of fuel-injection systems for internal-combustion engines [with list of references]: by A. G. Gelalles and E. T. Marsh.—Report 434. Lift and drag characteristics and gliding performance of autogiro as determined in flight [with list of references]: by John B. Wheatley.—Report 435. Fuel vaporization and its effect on combustion in high-speed compression-Ignition engine [with list of references]; by A. M. Rothrock and C. D. Waldron.—Report 436. Tests of nacelle-propeller combinations in various positions with reference to wings: [pt.] 2. Thick wing, various radial-engine cowlings. tractor propeller [with list of references]; by Donald H. Wood.—Report 437. Effect of area and aspect ratio on yawing moments of rudders at large angles of pitch on 3 fuselages [with list of references]; by Hugh L. Dryden and B. H. Monish.—Report 438. Experiments on distribution of fuel in fuel sprays [with list of references]; by Dana W. Lee.—Report 439. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack: 5, Spoilers and ailerons on rectangular wings [with references and bibliography]; by Fred E. Weick and Joseph A. Shortal.—Report 440. Mechanism of atomization accompanying solid injection [with list of references]; by R. A. Castleman, jr.—Aeronautical symbols.
Availability:
* For Sale by Superintendent of Documents. Cloth, $2.50.