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�������պ����ѧѧ�� 2002, Vol. 28 Issue (5) :601-604    DOI:
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Numerical Simulation of 3D Aerospike Nozzles
DAI Wu-ye, LIU Yu, MA Bin*
Beijing University of Aeronautics and Astronautics, School of Astronautics

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Abstract�� Based on three-dimensional Reynolds averaged Navier-Stokes equations and low Reynolds number ��k-� equations, a numerical program to simulate the 3D flowfield of aerospike nozzle was developed by employing two-order Non-oscillatory and Non-free-parameters Dissipative finite difference scheme. The 3D flowfield of a linear aerospike nozzle and a tile-shaped aerospike nozzle at different flight altitude were predicted. The results indicate that the pressure distribution on the plug of a tile-shaped aerospike nozzle have the advantage of load uniformity, and the cylindrical plug can load more than the planar plug under the same conditions.
Keywords�� rocket engines   three dimensional flow   computational fluid mechanics   aerospike nozzle     
Received 2001-08-16;
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����863�߼�����������������Ŀ(863-2-3-4-10); �ߵ�ѧУ��ʿѧ�Ƶ�ר����л���������Ŀ(2000000619)

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����Ҷ, ����, ���.��ʽ�����ά��������ֵģ��[J]  �������պ����ѧѧ��, 2002,V28(5): 601-604
DAI Wu-ye, LIU Yu, MA Bin.Numerical Simulation of 3D Aerospike Nozzles[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2002,V28(5): 601-604
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2002/V28/I5/601
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