Experimental analysis of heat flux to a blunt body in hypersonic flow with upstream laser energy deposition - Preliminary results

AIP Conference Proceedings

Volumn 830, Issue , 2006, Pages 163-171

  Salvador, I I ^a   Minucci, M A S ^b   Toro, P G P ^b   Oliveira, A C ^b   Channes Jr , J B ^b   Myrabo, L N ^c   Nagamatsu, H T ^c  

^a INSTITUTO NACIONAL DE PESQUISAS ESPACIAIS   (Brazil)

^b INSTITUTO DE ESTUDOS AVANÇADOS   (Brazil)

^c RENSSELAER POLYTECHNIC INSTITUTE   (United States)

Author keywords

Directed energy air spike; Experimental hypersonics; Transient heat transfer

Indexed keywords

EID: 33845435817     PISSN: 0094243X     EISSN: 15517616     Source Type: Conference Proceeding    
DOI: 10.1063/1.2203258     Document Type: Conference Paper

References (18)

1. Allen, H. J., Eggers Jr., A. J., "A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth's Atmosphere at High Supersonic Speeds", NACA-Report-1381, 1958.
2. Bogdonoff, S. M., Vas, I. E., Preliminary Investigations of Spiked Bodies at Hypersonic Speeds, Journal of the Aero/Space Sciences, v. 26, n. 2, p. 65-74, Feb. 1959.
3. th AIAA Plasmadynamics and Lasers Conference, Jun. 1994.
4. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Jun. 1994.
5. Head, D. R., "Theoretical Analysis of the Hypersonic 'Air Spike' Inlet", MSc Thesis, Rensselaer Polytechnic Institute, Troy, NY, 57p., Agosto 1994.
6. th Aerospace Sciences Meeting & Exhibit, Jan 1996.
7. Toro, P. G. P., "Experimental Pressure and Heat Transfer Investigation over a 'Directed Energy Air-Spike' Inlet at Flow Mach Numbers of 10 to 20, Stagnation Temperature of 1000K, and Arc Power up to 127kW", PhD Thesis, Rensselaer Polytechnic Inst, Troy, NY, August 1998.
8. Bracken, R. M., Myrabo, L. N., Nagamatsu, H. T., Meloney, E. D., Schneider, M. N., "Experimental Investigation of an Electric Arc Air-Spike with and without Blunt Body in Hypersonic Flow", AIAA Paper 2001-0796, 2001.
9. Minucci, M. A. S., Toro, P. G. P., Oliveira, A. C., Ramos, A. G., Chanes Jr., J. B., Pereira, A. L., Nagamatsu, H. T., Myrabo, L. N., "Laser-Supported Directed-Energy "Air Spike" in Hypersonic Flow", Journal of Spacecrafts and Rockets, Vol. 42, No. 1, pp. 51-57, 2005.
10. Nascimento, M. A. C., "Gaseous Piston Effect in Shock Tube/Tunnel When Operating in the Equilibrium Interface Condition", PhD Thesis, Inst. Tecnológico de Aeronáutica, Brazil, October 1997.
11. Watanuki, J.T., Oliva, J.L.S., Lobo, M.F.G., and Rodrigues, N.A.S., "Laser de CO2-Híbrido com Célula de Baixa Pressão Pulsada", Revista de Fisica Aplicada e Instrumentação, Vol. 3, No. 3, 1988, pp. 207-216.
12. th ISBEP, Japan, 2005.
13. Minucci, M. A. S., "An Experimental Investigation of a 2-D Scramjet Inlet at Flow Mach Numbers of 8 to 25 and Stagnation Temperatures of 800 to 4,100 K", Ph.D. Thesis, Rensselaer Polytechnic Institute, Troy, NY, May 1991.
14. Antonio carlos. . . .
15. Beck, J. V., Blackwell, B., St. Clair Jr., C. R., "Inverse Heat Conduction - Ill Posed Problems", John Wiley & Sons, New York, 1985.
16. Shultz, D. L., Jones, T.V., "Heat Transfer Measurements in Short Duration Facilities", AGARDograph No. 165, North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, February 1973.
17. Cook, W. J., Felderman, E. J., "Reduction of Data from Thin-Film Heat-Transfer Gages: A Concise Numerical Technique", AIAA Journal, vol. 4, no. 3, pp. 561-562, March 1966.
18. Takaki, R., Liou, M-S., "Parametric Study of Heat Release Preceding a Blunt Body in Hypersonic Flow", AIAA Journal, Vol. 40, No. 3, March 2002.