Numerical evaluation of further supersonic sections including ducted heat addition and nozzle flow-Reference-Cited by-同舟云学术

Numerical evaluation of further supersonic sections including ducted heat addition and nozzle flow

Published:1974 Issue:6 Volume:43 Page:395-412
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/BF00532138.pdf

Reference6 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; part of RAE Technical Report 69135 (1969)

2. Broadbent, E. G.: External heat addition for supersonic propulsion. Ing.-Arch. 40 (1971) pp. 168?187; part of RAE Technical Report 69135 (1969)

3. Broadbent, E. G.: Flowfield calculations for some supersonic sections with ducted heat addition. Ing.- Arch. 42 (1973) pp. 89?103; part of RAE Technical Report 71720 (1971)

4. Townend, L. H.: On hypersonic cruising aircraft which can have all leading edges swept. Part l: Design of air intakes. RAE Technical Report 67046 (1967)

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 9 (1968) pp. 329?456

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