Rotary Derivatives of a Delta Wing at Supersonic Speeds-Reference-Cited by-同舟云学术

Rotary Derivatives of a Delta Wing at Supersonic Speeds

Published:1948-11 Issue:455 Volume:52 Page:735-752
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Robinson A.

Abstract

SummaryThe rotary derivatives of a Delta wing pitching or rolling at supersonic speed are obtained in addition to the lift curve slope first given in an earlier investigation.

Publisher

Cambridge University Press (CUP)

Reference9 articles.

1. Supersonic wave drag of thin aerofoils;Puckett;Journal of the Aeronautical Sciences,1946

2. Ward G. N. . The pressure distribution on some flat laminar aerofoils at incidence at supersonic speeds. S.R.E. Airflow paper, 1946.

3. Glauert H. . The lift and pitching moment of an aerofoil due to a uniform angular velocity of pitch. R. and M. No. 1216, 1928.

4. Robinson A. . Aerofoil theory of a flat Delta wing at supersonic speeds. R.A.E. Report No. Aero 2151, 1946. (To be published in the R. and M. series.)

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1. Abraham Robinson, 1918-1974;Bulletin of the American Mathematical Society;1977

2. Impulse of the unsteady pressure acting on bodies in a liquid or gas;Fluid Dynamics;1972

3. Note on the Extension of Evvard’s Method to Wings with Subsonic Leading Edges Moving at Supersonic Speeds;Aeronautical Quarterly;1957-02

4. On Solutions to the Wave Equation in Hyperbolic Space;Journal of Applied Physics;1952-12

5. Airscrews at Supersonic Forward Speeds;Aeronautical Quarterly;1951-05