| Citation: | JIANG You-di, DONG Wei, CHEN Yong. Surface heat flux calculation of variable entropy flow for hypersonic blunt bodies[J]. Journal of Aerospace Power, 2008, 23(9): 1591-1594.
|
| [1] |
Cayzac R,Grignon C,Carette E.Navier-Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles[J].Aerospace Science and Technology,2006,10:374-384.
|
| [2] |
陈志敏,雷延花.天地往返运输器气动力和气动热工程计算方法研究[J].西北工业大学学报,2001,19(2):205-208.CHEN Zhimin,LEI Yanhua.On approximately predicting aerodynamic forces on and heating of fully-reusable launch vehicle[J].Journal of Northwestern Polytechnicai University,2001,19(2):205-208.(in Chinese)
|
| [3] |
吕丽丽.高超声速气动热工程算法研究[D].西安:西北工业大学,2005:18-20.LU Lili.Engineering studies of aerodynamic heating for hypersonic aircraft[D].Xi' an:Northwestern Poly technical University,2005:18-20.(in Chinese)
|
| [4] |
Zoby E V,Moss J N,Sutton K.Approximate convectiveheating equations for hypersonic flow[J].Journal of Spacecraft and Rockets,1981,18(I):64-70.
|
| [5] |
Quinn R D,Gong L.A method for calculating transient surface temperatures and surface heating rates for highspeed aireraft[R].NASA TP-209034,December 2000.
|
| [6] |
Fay J A,Riddell F R.Theory of stagnation point heat transfer in dissociated air[J].Journal of the Aeronautical Sciences,1958,25(2):73-85.
|
| [7] |
Beckwith I E,Gallagher J J.Local heat transfer and recovery temperatures on a yawed cylinder at a roach number of 4.15 and high reynolds numbers[R].NASA TR R-104,1961.
|
| [8] |
Frederick H C.Approximations for the thermodynamic and transport properties of high-temperature air[R].NASA TR R-50,1959.
|
| [9] |
Hamilton H H,Weilmuenster K J.Applicati on of axiymmetric analogue for calculating heating in three-dimensional fiows[R].AIAA-85 -0245.
|
| [10] |
Eckert E R G.Survey on heat transfer at high speeds[R].Wright-Air Development Center Technical Report,1954:54-70.
|
| [11] |
Anderson J D Jr.Hypersonic high temperature gas dynamics[M].New York:Mc Graw Hill Book Company,1988.
|
| [12] |
Cleary J W.Effects of angle of attack and bluntness on laminar heating-rate distributions of a 15 deg cone at a Math number of 10.6[R].NASA TN D-5450,October1969.
|
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