An exact numerical method of calculating inviscid heated flows in two dimensions with an example of duct flow-Reference-Cited by-同舟云学术

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An exact numerical method of calculating inviscid heated flows in two dimensions with an example of duct flow

Published:1971 Issue:1 Volume:40 Page:14-28
ISSN:0020-1154
Container-title:Ingenieur-Archiv
language:en
Short-container-title:Ing. arch

Author:

Broadbent E. G.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF00532199.pdf

Reference5 articles.

1. E. G. Broadbent, A class of twodimensional flows with heat addition, R.A.E. Technical Report 68005 (A.R.C. 30214), 1968.

2. A. W. Liepmann, A. Roshko, Elements of gas dynamics, New York 1957.

3. L. H. Townend, Ramjet propulsion for hypersonic aircraft, Euromech 3 Colloquim, Aachen 1966.

4. K. W. Mangler, Private communication.

5. E. G. Broadbent, External heat addition for supersonic propulsion, Ing.-Arch.

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1. References;The Aerodynamic Design of Aircraft;2012-09-15

2. Calculation of supersonic flows with heat addition;Philosophical Transactions of the Royal Society of London. Series A: Physical and Engineering Sciences;1991-04-15

3. Transonic thermal blooming due to an intense laser beam;Journal of Aircraft;1976-12

4. Flows with heat addition;Progress in Aerospace Sciences;1976-01

5. Stationäre, räumliche Strömung mit Energiezufuhr;Gasdynamik der Verbrennung;1975

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