Experimental investigation of hypersonic ‘Directed-energy air spike’ inlet at mach 10 - 20

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Toro, P G P ^a   Myrabo, L N ^a   Nagamatsu, H T ^a  

^a RENSSELAER POLYTECHNIC INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AERODYNAMICS; AEROSPACE ENGINEERING; AUTOMOBILE BODIES; HYPERSONIC FLOW; MACH NUMBER; SHOCK WAVES; VEHICLE TRANSMISSIONS;

DIRECTED ENERGY; ELECTRIC POWER; EXPERIMENTAL INVESTIGATIONS; HYPERSONIC SPEED; MOVING VEHICLES; PILOT PRESSURE; STAGNATION POINTS; SURFACE PRESSURES;

HYPERSONIC INLETS;

EID: 84983175032     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Myrabo, L. and Raizer, Yu. P. "Laser Induced Air Spike for Advanced Transatmospheric Vehicles," AIAA-94-2451, June, 1994.
2. Bogdonoff, S. and Vas, I. "Preliminary Investigations of Spiked Bodies at Hypersonic Speeds," J. of AeroSpace Sciences, Vol. 26, №2, Feb., 1959, pp. 65-74.
3. Crawford, D. "Investigation of the Flow over a Spiked-Nose Hemisphere-Cylinder," NASA TN D-118, December, 1959.
4. Maull, D. "Hypersonic Flow over Axially Symmetric Spiked Bodies," J. of Fluid Mechanics, Vol. 8, № 4, pp. 584-592.
5. Wood, C. "Hypersonic Flow over Spiked Cones," J. of Fluid Mechanics, Vol. 12, № 4, pp. 614-624.
6. Calarese, W. and Hankey, W. "Modes of Shock-Wave Oscillations on Spiked-Tipped Bodies," AIAA Journal, Vol. 23, № 2, Feb., 1985, pp. 185-192.
7. Minucci, M.A.S., and Nagamatsu, H.T., "Hypersonic Shock Tunnel Testing at an Equilibrium Interface condition of 4100K," Journal of Thermophysics and Heat Transfer, vol. 7, 1993, pp. 251-260.
8. Lomax, H. and Inouye, M. "Numerical Analysis of Flow Properties about Blunt Body moving at Supersonic speeds in an Equilibrium Air," NASA TR-R-204, 1964.
9. Lees. L. "Hypersonic Flow," 5lh International Aeronautical Conference, L.A., pp. 241-276, 1955.
10. Nagamatsu, H.T., Geiger, R.E. and Sheer Jr., R.E. "Real Gas Effects in Flow over Blunt Bodies at Hypersonic Flow," J. of the Aero/Space Sciences, vol. 27, no. 4, Apr. 1960
11. Nagamatsu, H.T., Geiger, R.E. and Sheer, R.E.Jr. "Hypersonic Shock Tunnel," ARS Journal, vol. 29, 1959, pp. 332-340.
12. Kubota, H., Watanulci, T., Matsumoto, S., Fujita, M. "Effect of Spike Attached on a Hemisphere in Hypersonic Flow," Proceedings of the 19th International Symposium on Space Technology, and Science, Yokohama, 1994, pp. 363-369.
13. Fujita, M. and Kubota, H. "Numerical Simulation of Flowfield over a Spiked Blunt-Nose," Computational Fluid Dynamics Journal, Vol. 1, № 2, July 1992,pp. 187-195.
14. Yamauchi, M., Fujii, K., and Higashino, F. "Numerical Investigation of Supersonic Flows Around a Spiked Blunt Body," J. of Spacecraft and Rockets, vol. 32, no. 1, Jan./Feb. 1955.
15. Moraes Jr., P. and Ganzer, U. ‘The Flowficld of a Sonic Jet Exhausting against a Supersonic Flow," VTU COBEM, pp. 113- 115, Brazil, Dec. 1985.
16. Moraes Jr., P. "Pressure Measurements in a Supersonic Counter-Flow," IX COBEM, Brazil, Dec. 1987.
17. Levin, V. and Tercnteva, L. "Supersonic Flow over a Cone with Heat Release in the Neighborhood of the Apex," Izvestiya Rossiiskoi Akademii Nauk Mekhanika Zhidkosti i Gaza, № 2, March-April, 1993, pp. 110-114.
18. Private communication with Yu. P. Raizer.
19. Marsh, J.J., Myrabo, L.N., Messitt, D.G., Nagamatsu, H.T "Experimental Investigation of the Hypersonic Air Spike Inlet at Mach 10," AIAA Paper 96-0720, Jan., 1996.
20. Myrabo, L., Seo, J., Head, D., March, J. and Cassenti, B. ‘Thermal Management System for an Ultralight Microwave Propelled Transatmospheric Vehicle," AIAA 94-2924, Jun. 1994.
21. March, J.J., Myrabo, L.N., Messitt, D.G., Nagamatsu, H.T. and Raizer, Y.P. "Experimental Investigation of the Hypersonic "Air Spike" Inlet at Mach 10," AIAA 96-0721, Jan. 1996.
22. Minucci, M. A. S. "An Experimental Investigation of a 2-D Scramjet Met at flow Mach numbers of 8 to 25 and Stagnation Temperatures of 800 to 4,100 K," AIAA Paper 91-5018, Dec., 1991.