Mean and fluctuating pressure field in boat-tail separated flows at transonic speeds
Author:
Affiliation:
1. National Aerospace Labs., Bangalore, India
2. Indian Inst. of Science, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-582
Reference20 articles.
1. Coe, C. F.(1962)The effect of some variations in launch vehicle nose shape on steady and fluctuating pressure attransonic speeds,NASA TMX- 646
2. Reflexion of an oblique shock wave by a turbulent boundary layer
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