1[1]Sook-Ying Ho,Allan Paull.Coupled thermal,structural and vibrational analysis of a hypersonic engine for flight test[J].Aerospace Science and Technology,2006,10:420-426. 被引量：1
2[2]Roxan Cayzac,Christophe Grignon,Eric Carette.Navier-Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles[J].Aerospace Science and Technology,2006,10:374-384. 被引量：1
3[3]D J.Kinney Aero-thermodynamics for concept-ual design[R].AIAA-2004-0041,2004. 被引量：1
4[4]K E Wurster,E V Zoby,Thomp son R A.Flowfield and vehicle parameter influence on results of engineering aerothermal methods[J].Journal of Spacecraft,1991,28(1):6-22. 被引量：1
5[5]H H Hamilton,A G Franceis.Approximate method for calculating heating rates on three-dimensional vehicles[J].Journal of Spacecraft and Rockets,1994,31(3):345-354. 被引量：1
6[7]Quinn,D Robert.and Leslie Gong.A method for calculating transient surface temperatures and surface heating rates for high-speed aircraft[R].NASA TP--2000-209034,December 2000. 被引量：1
7[8]Hansen,C,Frederick.Approximations for the Thermodynamic and Transport Properties of High-Temperature Air[R].NASA TR R-50,1959. 被引量：1
8[9]H Harris Hamilton Ⅱ.Calculation of laminar heating rates on three-dimensional configura-tions using the axisymmetric analogue[R].NASA TP-1698,September 1980. 被引量：1
