Effect of Eccentricity on the Thermal Behaviour of A Re-Entry Vehicle With Concave Windward Surface
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-16-0698-4_16
Reference4 articles.
1. Stallings RL, Burbank PB (1959) Heat transfer and measurements on a concave nose cylinder for a mach number range of 2.49–4.44. NASA TM-X-221
2. Saravanan S, Jagadeesh G, Reddy KPJ (2009) Investigation of missile shaped body with forward facing cavity at Mach 8. J Spacecraft Rockets 46(3)
3. Engblom et al (1996) Experimental and numerical study of the hypersonic forward facing cavity. J. Spacecrafts Rockets 33(3)
4. Engblom WA, Goldstein DB (1996) Nose-tip surface heat reduction mechanism. J Thermo Phys Heat Transf 10(4)
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