Free-flight measurements of convective heat transfer rates in hypersonic ballistic-range environments

Collection of Technical Papers - 39th AIAA Thermophysics Conference

Volumn 2, Issue , 2007, Pages 1164-1173

  Wilder, M C ^a,b,c   Reda, D C ^a,c,d   Bogdanoff, D W ^a,c,e   Prabhu, D K ^a,c,e  

^a NASA AMES RESEARCH CENTER   (United States)

^b Reacting Flow Environments Branch   (United States)

^c AIAA   (United States)

^d Space Technology Division ^*  (United States)

^e ELORET CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FREE-FLIGHT MEASUREMENTS; NAVIER-STOKES COMPUTATIONS; STATIC PRESSURE; TEST GAS COMPOSITION;

HEAT TRANSFER; HYPERSONIC FLOW; INFRARED IMAGING; NAVIER STOKES EQUATIONS;

FLIGHT DYNAMICS;

EID: 35748962620     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Strawa, A.W., Chapman, G.T., Canning, T.N., and Arnold, J.O., "The Ballistic Range and Aerothermodynamic Testing," AIAA 88-2015, 15th Aerodynamic Testing Conference, San Diego, CA, May 18-20, 1988.
2. Page, W.A., "A Survey of Thermal Radiation Studies of Ablating Bodies in the Ballistic Range," NASA TN D-3741, Feb. 1967.
3. Cooper, D.M., "Equilibrium Air Radiation from Shock Layers at 11.3 km/sec," AIAA Journal, Vol.4, No. 12, Dec. 1966, pp. 2125-2130.
4. Compton, D.L. and Cooper, D.M, "Free-Flight Measurements of Stagnation-Point Convective Heat Transfer at Velocities to 41,000 ft/sec," NASA TM D-2871, June 1965.
5. Compton, D.L. and Cooper, D.M., "Measurements of Radiative Heating on Sharpe Cones," AIAA Journal, Vol. 3, No. 1, Jan. 1965, pp. 107-114.
6. DeRose, CE., "Trim Attitude, Lift and Drag of The Apollo Command Module with Offset Center-Of-Gravity Positions at Mach Numbers to 29," NASA TN D-5276, June 1969.
7. th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 2000.
8. Brown, J., Yates, L., Bogdanoff, D., Chapman, G., Loomis, M., and Tam, T., "Free Flight Testing in Support of the Mars Smart Lander Aerodynamics Database," AIAA 2002-4410, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Monterey, CA, Aug. 2002.
9. Reda, D. C., Wilder, M. C., Bogdanoff, D.W., and Olejniczak, J., "Aerothermodynamic Testing of Ablative Reentry Vehicle Nosetip Materials in Hypersonic Ballistic-Range Environments," AIAA 2004-6829, 1st U. S. Air Force Developmental Test & Evaluation (DT&E) Summit, Woodland Hills, CA, November 16-18, 2004.
10. Cornelison, C.J., "Status Report For The Hypervelocity Free-Flight Aerodynamic Facility," 48th Meeting of the Aeroballistic Range Association, Austin, TX, Nov. 1997.
11. Canning, T.N., Seiff, A., and James, C.S. (Ed.) "Ballistic Range Technology," AGARDograph No. 138, 1970.
12. Hill, P. R., Adamson, D., Foland, D. H., and Bressette, W. E., "High-temperature oxidation and ignition of metals," NACA-RM-L55L23b, March 26, 1956.
13. Touloukian, Y. S., series editor, "Thermophysical properties of matter," Purdue University, Thermophysical Properties Research Center, New York, IFI/Plenum, 1970-[79].
14. Schultz, D.L., and Jones, T.V., "Heat-transfer Measurements in Short-duration Hypersonic Facilities," AGARDograph No. 165, 1973.
15. Fay, J.A., and Riddell, F.R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," J. Aero. Sci., Vol. 25, No. 2, February 1958, pp. 73-85.
16. Wright, M. J., Candler, G. V., and Bose, D., "Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp. 1603-1609.
17. Detra, R. W., Kemp, N. H., and Riddell, F. R., "Addendum to 'Heat Transfer to Satellite Vehicles Re-Entering the Atmosphere'," Jet Propulsion, Vol. 27, Dec. 1957, pp. 1256-1257.
18. Hoshizaki, H., "Heat Transfer in Planetary Atmospheres at Super-Satellite Speeds," ARS Journal, Vol. 32, Oct. 1962, pp. 1542-1544.
19. Yee, L., Bailey, H.E., and Woodward, H.T., "Ballistic range measurements of stagnation-point heat transfer in air and in carbon dioxide at velocities up to 18,000 feet per second," NASA TN D-777, March 1961.