External heat addition for supersonic propulsion-Reference-Cited by-同舟云学术

External heat addition for supersonic propulsion

Published:1971 Issue:3 Volume:40 Page:168-187
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/BF00532148.pdf

Reference14 articles.

1. E. G. Broadbent, An exact numerical method of calculating inviscid heated flows in two dimensions with an example of duct flow, Ing.-Arch. 40 (1971) p. 14.

2. K. Oswatitsch, Antriebe mit Heizung bei Überschallgeschwindigkeit, DVL-Bericht 90 (1959).

3. H. Lomax, Twodimensional, supersonic, linearised flow with heat addition, NASA Memo. 1-10-59A, NASA TIL 6196 (1959).

4. A. Mager, Supersonic airfoil performance with small heat addition, IAF preprint 768. J. Aero Sci. 26 (1959) p. 99.

5. R. W. Linden, R. J. Flaherty, S. H. Maslen, Analysis and evaluation of supersonic under wing heat addition, NASA TIL 6345, NASA Memo. 3-17-59E (1959).

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

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

3. Numerical evaluation of further supersonic sections including ducted heat addition and nozzle flow;Ingenieur-Archiv;1974

4. Shockless flows with heat addition in two dimensions;Acta Mechanica;1973-03

5. Flowfield calculations for some supersonic sections with ducted heat addition;Ingenieur-Archiv;1973