Mean and Fluctuating Pressure in Boat-Tail Separated Flows at Transonic Speeds
Author:
Affiliation:
1. National Aerospace Laboratories, Bangalore 560 017, India
2. Indian Institute of Science, Bangalore 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3826
Reference15 articles.
1. Dynamic response of a hammerhead launch vehicle wind-tunnel model
2. Progress on the launch-vehicle buffeting problem
3. Flow Quality Improvements in a Blowdown Wind Tunnel
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