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�������պ����ѧѧ�� 1998, Vol. 24 Issue (2) :189-192    DOI:
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Calculating Method of Aerodynamic Heating for Space Shuttles
Shen Xialing*
Beijing University of Aeronautics and Astronautics,Dept. of Flight Vihicle Design and Applied Mechanics

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Abstract�� Approximate methods for calculating aerodynamic heating rates on space shuttles are discussed.Various methods are given for predicting the heating rate at axisymmetric stagnation points,general three dimensional stagnationpoints and the leading edge stagnation point of wings.Numerous laminar and turbulent heating techniques for flat plates and cones are analyzed and compared.A brief review of some methods is presented to predict heating rate for winward centerline and lateral direction off the symmetry plane.The results show that the methods are simpler and can guarantee enought precision for predicting aerodynamic heating environment of space shuttles.
Keywords�� space shuttles   aerodynamic heating   hypersonic flow   engineering calculation     
Received 1996-12-04;
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������.����ɻ��������ȼ���[J]  �������պ����ѧѧ��, 1998,V24(2): 189-192
Shen Xialing.Calculating Method of Aerodynamic Heating for Space Shuttles[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 1998,V24(2): 189-192
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