fa en fa ar fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa ur fa fa fa fa fa fa fa en fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa ur fa fa en fa en it en azb en ar en en en en en en en en en en en en en en en en en en en en fa azb fa fa el fa fa fa it id en en id bo en en fa ar fa de id fa de bo fa de en fa de en fa fa fa fa fa fa fa fa fa fa ar fa fa fa fa fa fa fa de
Effects of pulsed counter flow jets on aerothermodynamics performance of a Re-Entry capsule at supersonic flow
Seyed Arash Seyed ShamsTaleghani 3
[1] Stadler, J. R., M. Inouye. “A Method of Reducing Heat Transfer to Blunt Bodies by Air Injection.” NACA, May, 1956.
[2] Ferri, A., M. H. Bloom. “Cooling by Jets Directed Upstream in Hypersonic Flow.” WADC Technical Note 56-382, Sept. 1957.
[3] Resler Jr., E. L., W. R. Sears. “The Prospects for Magneto-Aerodynamics.” Journal of the Aeronautical Sciences, Vol. 25, April 1958, pp. 235-245.
[4] Charczenco, N., K. W. Hennessey. “Investigation of a Retro-Rocket Exhausting from the Nose of a Blunt Body into a Supersonic Free Stream.” NASA TND-75 1, 1961.
[5] Warren, C. H. E. “An Experimental Investigation of the Effect of Ejecting a Coolant Gas at the Nose of a Bluff Body.” Journal of Fluid Mechanics, Vol. 2, No. 8, 1960, pp 400-417.
[6] Grimaud, J. E., L. C. McRee. “Experimental Data on Stagnation-Point Gas Injection Cooling on Hemispherical-Cone in a Hypersonic Arc Tunnel.” NASA TM X-983, July 1964.
[7] Beckwith, I. E., D. M. Bushnell. “Effect of Intermittent Water Injection on Aerodynamic Heating of a Sphere-Cone at Flight Velocities to 18000 Feet per Second.” NASA TM X-1128, 1965.
[8] Keyes, J. W., J. N. Hefner. “Effects of Forward-Facing Jets on Aerodynamic Characteristics of Blunt Configuration at Mach 6.” Journal of Spacecraft, Vol. 4, No. 4, April 1967, pp 533-534.
[9] Bushnell, D. M., J. K. Huffinan. “Forward Penetration of Liquid Water and Liquid Nitrogen from the Orifice at the Stagnation Point of a Hemispherically Blunted Body in Hypersonic Flow.” NASA TM X-1493, March1968.
[10] Jarvinen, P. O., R. H. Adams. “The Effects of Retrorockets on the Aerodynamic Characteristics of Conical Aeroshell Planetary Entry Vehicles.” AIAA Paper 70-219, January 1970.
[11] Shang, J. S., J. Hayes, K. Wurtzler, W. Strang. "Jet spike bifurcation in high speed flow." AIAA J., 39, 2001, pp. 1159-1165.
[12] Veukumar, B., G. Jagadeesh, K. P. J. Reddy, "Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow." Phys. Fluids, 18, 2006, pp. 81041-81044.
[13] Daso, E. O., W. Beaulieu, J. O. Hager. “Prediction of Drag Reduction in Supersonic and Hypersonic Flow with Counter-flow Jets.” AIAA 2002-5 115.
[14] Daso, E. O., V. E. Pritchett, T. S.  Wang, et al. "Dynamics of shock dispersion and interactions in supersonic freestreams with counterflowing jets." AIAA Journal, 47(6), 2009, pp. 1313-1326.
[15] Chen, L. W., G. L. Wang, X. Y. Lu. "Numerical investigation of a jet front a blunt body opposing a supersonic flow." J. Fluid Mech., 684, 2011, pp. 85-110.
[16] Chao-Ying, Zh. "Numerical investigation on the drag and heat flux reduction of a supersonic reentry capsule with a counter-flow jet." Information Technology Journal 11(12), 2012, pp. 1705-1713.
[17] Zheng, Y., N. A. Ahmed, W. Zhang. “Heat dissipation using minimum counter flow jet ejection during spacecraft re-entry.” Procedia Engineering 49, 2012, pp. 271-279.
[18] Wilson, F., N. Santos. "Gas-Surface interaction impact on aerodynamic heating of a reentry Brazilian capsule." Combustion and Propulsion Laboratory (LPC), 2013, INPE 12630-000.
[19] Shyam, K., M. Singh, Sh. Jaiswal, G. Sh. Kanday. “Numerical Study on Aerodynamic Wave Drag Reduction by Counterflow Supersonic Jet in Hypersonic Flow.” International Journal of Science and Research, Vol. 4, Issue 3, March 2015.
[20] Wei, H. “A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations.” Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 16(7), 2015, pp. 551-561.
دوره 5، شماره 1 - شماره پیاپی 1
اصل مقاله 4.1 MB
ارجاع به این مقاله
تعداد مشاهده مقاله: 1,197
تعداد دریافت فایل اصل مقاله: 1,209
عبدالهی, سهیلا, مردانی, عباس, & سید شمس طالقانی, سید آرش. (1395). تأثیر جت خلاف جریان پالسی بر عملکرد ائروترمودینامیکی برای یک کپسول بازگشتی مافوق صوت. دانش و فناوری هوافضا, 5(1), 55-65.
سهیلا عبدالهی; عباس مردانی; سید آرش سید شمس طالقانی. "تأثیر جت خلاف جریان پالسی بر عملکرد ائروترمودینامیکی برای یک کپسول بازگشتی مافوق صوت". دانش و فناوری هوافضا, 5, 1, 1395, 55-65.
عبدالهی, سهیلا, مردانی, عباس, سید شمس طالقانی, سید آرش. (1395). 'تأثیر جت خلاف جریان پالسی بر عملکرد ائروترمودینامیکی برای یک کپسول بازگشتی مافوق صوت', دانش و فناوری هوافضا, 5(1), pp. 55-65.
عبدالهی, سهیلا, مردانی, عباس, سید شمس طالقانی, سید آرش. تأثیر جت خلاف جریان پالسی بر عملکرد ائروترمودینامیکی برای یک کپسول بازگشتی مافوق صوت. دانش و فناوری هوافضا, 1395; 5(1): 55-65.