Flowfield calculations for some supersonic sections with ducted heat addition
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF00533073.pdf
Reference5 articles.
1. Broadbent, E. G.: An exact numerical method of calculating inviscid heated flows in two dimensions with an example of duct flow. Ing.-Arch. 40 (1971) pp. 14?28.
2. Broadbent, E. G.: External heat addition for supersonic propulsion. Ing.-Arch. 40 (1971) pp. 168?187.
3. Oswatitsch, K.: Pressure recovery for missiles with reaction propulsion at high supersonic speeds. (The efficiency of shock diffusers.) NACA-TM-1140 (1947).
4. Küchemann, D.: Hypersonic aircraft and their aerodynamic problems. Progress in Aeronautical Sciences, Vol. 6 (1965).
5. Küchemann, D.; Weber, J.: An analysis of some performance aspects of various types of aircraft designed to fly over different ranges at different speeds. Progress in Aeronautical Sciences, Vol. 9 (1968).
Cited by 3 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;The Aerodynamic Design of Aircraft;2012-09-15
2. Transonic thermal blooming due to an intense laser beam;Journal of Aircraft;1976-12
3. Numerical evaluation of further supersonic sections including ducted heat addition and nozzle flow;Ingenieur-Archiv;1974
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