Integrated supersonic wind tunnel nozzle

Author:

SHEN Junmou,DONG Jingang,LI Ruiqu,ZHANG Jiang,CHEN Xing,QIN Yongming,MA Handong

Funder

CAAA

National Nature Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference22 articles.

1. Approximate for plug nozzle;Gianfranco;AIAA J,1964

2. A history of aerodynamics and its impact on flying machine;Anderson,1997

3. Foelsch K. A new method of designing two dimensional Laval nozzles for a parallel and uniform Jet. California: North American Aviation; 1946. Report No.: NA-46-235-1.

4. Cresci RJ. Tabulation of coordinates for hypersonic axisymmetric nozzles. Part I – Analysis and coordinates for test section Mach numbers of 8, 12, and 20. Ohio: Wright Air Development Center; 1958. Report No.: WADD-TN-58-300.

5. Aerodynamic design of axisymmetric hypersonic wind-tunnel nozzles;Sivells;J Spacecraft Rockets,1970

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