Report. 23d annual report of National Advisory Committee for Aeronautics, [fiscal year] 1937, including Technical reports 577-611.
Publication Title:
Report. 23d annual report of National Advisory Committee for Aeronautics, [fiscal year] 1937, including Technical reports 577-611.
Display Title:
Report. 23d annual report of National Advisory Committee for Aeronautics, [fiscal year] 1937, including Technical reports 577-611.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1938
Publish Date ISO Format:
1938-01-01T00:00:00Z
Publication Start:
19380101
Publication End:
19381231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1938
SuDoc number:
Y 3.N 21/5:1/937-2
Description:
x+742+[1] 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.—23d annual report.—Report 577. Prechamber compression-ignition engine performance [with references and bibliography]: by Charles S. Moore and John H. Collins, jr.—Report 578. Flight measurements of dynamic longitudinal stability of several airplanes and correlation of measurements with pilots' observations of handling characteristics [with list of references]; by Hartley A. Soulé.—Report 579. Study of 2-control operation of airplane [with list of references]; by Robert T. Jones.—Report 580. 2-control operation of airplane [with list of references]; by Robert T. Jones.—Report 580. Heat transfer to fuel sprays injected into heated gases [with list of references]; by Robert F. Selden and Robert C. Spencer.—Report 581. Measurements of intensity and scale of wind-tunnel turbulence and their relation to critical Reynolds number of spheres [with list of references]; by Hugh L. Dryden. G. B. Schubauer. W. C. Mock. jr., and H. K. Skramstad.—Report 582. Theory for primary failure of straight centrally loaded columns [with list of references]; by Eugene E. Lundquist and Claude M. Fligg.—Report 583. Rolling friction of several airplane wheels and tires and effect of rolling friction on take-off [with one referencel; by J. W. Wetmore. —Report 584. Strength of welded aircraft joints [with references and bibliography]; by W. C. Brueggeman.—Report 585. Span load distribution for tapered wings with partial-span flaps [with list of references]; by H. A. Pearson.—Report 586. Ai foil section characteristics as affected by variations of Reynolds number [with list of references]; by Eastman N. Jacobs and Albert Sherman.—Report 587. Blower doling of finned cylinders [with list of references]; by Oscar W. Schey and Herman H. Ellerbrock. jr.— Report 588. Fuel spray and flame formation in compression-ignition engine employing air flow [with list of references]; by A. M. Rothrock and C. D. Waldron.—Report 589. Analysis of lateral stability in nower-off flight with charts for use in design land with list of references]; by Charles H. Zimmerman.—Report 590. Pressure-distribution measurements on O-2H airplane in flight [with list of references]; by H. A. Pearson.—Report 591. Analytical and experimental study of effect of periodic blade twist on thrust torque, and flapping motion of autogiro rotor [with list of references]; by John B. Wheatley.—Report 592. Full-scale tests of N. A. C. A. cowlings [with list of references 1; by Theodore Thendorsen. M. J. Brevoort. and George W. Stickle.—Report 593. Cooling of airplane engines at low air six eds [with list of references)]; by Theodore Tbeodorsen. M. J. Brevoort. and George W. Stickle.—Report 594. Characteristics of 6 propellers including high-speed range [with list of references]; by Theodore Theodorsen, George W. Stickle, and M. J. Brevoort.—Report 595, Full-scale tests of new type N. A. C. A. nose-slot cowling [with list of references]; by Theodore Theodorsen, M. J. Brevoort. George W. Stickle, and M. N. Goueh.—Report 596 Cooling tests of single-row radial engine with several N. A. C. A. cowlings [with list of references]; by M. J. Brevoort. George W. Stickle, and Herman H. Ellerbrock. jr.—Report 597. Air propellers in yaw [with list of references]; by E. P. Lesley. George F. Worley and Stanley Moy.—Report 598. Alternating-current equipment for measurement of fluctuations of air speed in turbulent flow [with list of references]; by W. C. Mock. jr.—Report 599. Flight tests of drag and torque of propeller in terminal-velocity dives [with list of references]; by Richard V. Rhode and Henry A. Pearson.—Report 600. Analysis of factors that determine periodic twist of autogiro rotor blade, with comparison of predicted and measured results [with list of references]; by John B. Wheatley.—Report 601. Torsion tests of tubes [with list of references]; by Ambrose H. Stang, Walter Ramberg, and Goldie Back—Report 602. Wind-tunnel and flight tests of slot-lip ailerons [with list of referencesl; by Joseph A. Shortal.—Report 603 Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps [with list of references]; by Robert C. Platt and Joseph A. Shortal.—Report 604. Pressure-distribution measurements at large angles of pitch on fins of different spar-chord ratio on 1/40-scate model of U. S. airship Akron [with list of references]; by James G. Mcllugh—Report 605. Résumé and analysis of N. A. C. A. lateral control research [with list of references]; by Fred E. Weick and Robert T. Jones.—Report 600. Electrical thermometers for aircraft [with references and bihlioeraphy]; by John B. Peterson and S H. J. Womack—Report 607. Spinning characteristics of XN2Y-1 airplane obtained from spinning balance and compared with results from spinning tunnel and from flight tests [with list of references]; by M J. Bamber and R. O. House—Report 608. Stress analysis of beams with shear deformation of flanges [with list of references]; by Paul Kuhn— Report 609. Experimental investigation of wind-tunnel interference on downwash behind airfoil [with list of referencesl; by Abe Silverstein and S. Katzoff.—Report 610 Tests of related forward-camber airfoils in variable-density wind tunnel [with list of references]; by Eastman N. Jacobs. Robert M. Pinkerton, and Harry Greenberg—Report 611. Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps [with list of references]; by Carl J. Wenzlnger.—Aeronautic symbols.
Availability:
* For Sale by Superintendent of Documents. Cloth, $2.50.