Wind Tunnel Tests on Aerodynamic Characteristics of Advanced Solid Rocket
Author:
Affiliation:
1. JAXA/JEDI
2. JAXA/ISAS
3. JAXA Advanced Solid Rocket Team
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/astj/9/0/9_0_9/_pdf
Reference8 articles.
1. 5)Forsythe, J.R., Hoffmann, K.A., Cummings, R.M., and Squires, K.D.: Detached-Eddy Simulation with Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow, J. Fluids Engineering, 124 (2002), pp.911-923.
2. An Experimental Study on Base Pressure Correction for Bluff-Base Bodies Using Magnetic Suspension and Balance System
3. 7)Pope, A. and Goin, K.L.: High-Speed Wind Tunnel Testing, John Wiley & Sons, Inc., New York, 1965, p.323.
4. 9)Garbaruk, A., Shur, M., Strelets, M., and Spalart, P.R.: Numerical Study of Wind-Tunnel Walls Effects on Transonic Airfoil Flow, AIAA J., 41 (2003), pp.1046-1054.
5. 10)Roshko, A. and Thomke, G.J.: Observations of Turbulent Reattachment behind an Axisymmetric Downstream- Facing Step in Supersonic Flow, AIAA J., 4 (1966), pp.975-980.
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