Source-superposition method of solution of a periodically oscillating wing at supersonic speeds-Reference-Cited by-同舟云学术

Source-superposition method of solution of a periodically oscillating wing at supersonic speeds

Published:1951 Issue:1 Volume:9 Page:31-45
ISSN:0033-569X
Container-title:Quarterly of Applied Mathematics
language:en
Short-container-title:Quart. Appl. Math.

Author:

Stewart H. J.,Li Ting-Yi

Publisher

American Mathematical Society (AMS)

Subject

Applied Mathematics

Link

http://www.ams.org/qam/1951-09-01/S0033-569X-1951-42272-8/S0033-569X-1951-42272-8.pdf

Reference8 articles.

1. A linearized solution for time-dependent velocity potentials near three-dimensional wings at supersonic speeds;Evvard, John C.;Tech. Notes Nat. Adv. Comm. Aeronaut.,1948

2. Distribution of wave drag and lift in the vicinity of wing tips at supersonic speeds;Evvard, John C.;Tech. Notes Nat. Adv. Comm. Aeronaut.,1947

3. Theoretical lift distribution and upwash velocities for thin wings at supersonic speeds;Evvard, John C.;Tech. Notes Nat. Adv. Comm. Aeronaut.,1947

4. Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream;Garrick, I. E.;Tech. Notes Nat. Adv. Comm. Aeronaut.,1947

5. The lift of a delta wing at supersonic speeds;Stewart, H. J.;Quart. Appl. Math.,1946

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. REFERENCES;Wing Theory in Supersonic Flow;1969

2. Application of the Compensation Theorem to the Modification of Redundant Structures;Journal of the Aeronautical Sciences;1953-10

3. On an Integral Equation in the Supersonic Oscillating Wing Theory;Journal of the Aeronautical Sciences;1953-10

4. A general solution for the rectangular airfoil in supersonic flow;Quarterly of Applied Mathematics;1953

5. ON THE LINEARIZED POTENTIAL THEORY OF UNSTEADY SUPERSONIC MOTION. II;The Quarterly Journal of Mechanics and Applied Mathematics;1952