Author: National Advisory Committee for Aeronautics / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publish Year Decade 1950 - 1959

11. Technical notes. 4346. Approximate method for calculating motions in angles of attack and sideslip due to step pitchingand yawing-moment inputs during steady roll [with list of references]; by Martin T. Moul and Teresa R. Brennan.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

12. Technical notes. 4358. Supersonic wave interference affecting stability [with list of references]; by Eugene S. Love.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

13. Technical notes. 4371. Some observations relating to recovery of internal friction during fatigue of aluminum [with list of references]; by S. R. Valluri.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

14. Technical notes. 4375. Approximate solutions of class of similarity equations for 3-dimensional, laminar, incompressible boundary-layer flows [with list of references]; by Arthur G. Hansen and Howard Z. Herzig.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

15. Technical notes. 4388. Effects of nose angle and Mach numbers on transition on cones at supersonic speeds [with list of references]; by K. R. Czarnecki and Mary W. Jackson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

16. Technical notes. 4390. Effects of frequency and amplitude on yawing derivatives of triangular, swept, and unswept wings and of triangular-wing-fuselage combination with and without triangular tail performing sinusoidal yawing oscillations [with list of references]; bv William Letko and Herman S. Fletcher.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

17. Research memorandum RM (series). L58C28a. Landing and taxiing tests over various types of runway lights [with list of references]; by Robert C. Dreher and Sidney A. Batterson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 26, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

18. Research memorandum RM (series). [Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]. A58C21. Static longitudinal characteristics of twisted and cambered 45° sweptback wing at Mach numbers up to 0.96 [with list of references]; by Robert I. Sammonds and Robert M. Reynolds.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Washington, Aug. 11, 1958
SuDoc number:: Y 3.N 21/5:15/A 58C 21

19. Technical notes. 1320. Compressible laminar flow and heat transfer about rotating isothermal disk [with list of references]; by Simon Ostrach and Philip R. Thornton.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

20. Technical notes. 4016. Some factors affecting variation of pitching moment with sideslip of aircraft configurations [with list of references]; by Edward C. Polhamus.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

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