Transient source, doublet and vortex solutions of the linearized equations of supersonic flow-Reference-Cited by-同舟云学术

Transient source, doublet and vortex solutions of the linearized equations of supersonic flow

Published:1950-06-22 Issue:1068 Volume:202 Page:40-53
ISSN:0080-4630
Container-title:Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences
language:en
Short-container-title:Proc. R. Soc. Lond. A

Author:

Abstract

By introducing the Heaviside step function as the time variation of the fundamental source solution of the wave equation of compressible gas flow, a family of ‘transient’ source and doublet solutions is derived, together with a generalization of the vortex, and their more interesting properties are explored. These results are applicable to unsteady supersonic aerofoil theory and similar problems.

Publisher

The Royal Society

Subject

Pharmacology (medical)

Link

https://royalsocietypublishing.org/doi/pdf/10.1098/rspa.1950.0084

Reference5 articles.

1. Evvard J. C. 1948 Tech. Notes Nat. Adv. Comm. Aero. Wash. no. 1699.

2. Heaslet M. A. & Lomax H. 1947 Tech. Notes Nat. Adv. Comm. Aero. Wash. no. 1616.

3. Lighthill M. J. 1944 Rep. Memor. Aero. Res. Comm. Lond. no. 2001.

4. Robinson A. 1947 College of Aeronautics Cranfield Rep. no. 9.

5. Proc. Roy;Strang W. J.;Soc. A,1948

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1. Singularities of wavefields and sonic boom;Wave Motion;2008-01

2. William John Strang, C.B.E., F.R.Eng., F.R.Ae.S. 29 June 1921 – 14 September 1999;Biographical Memoirs of Fellows of the Royal Society;2001-01

3. Mathematical research at the Aeronautical Research Laboratories 1939–1960;The Journal of the Australian Mathematical Society. Series B. Applied Mathematics;1989-04

4. REFERENCES;Wing Theory in Supersonic Flow;1969

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