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Optimal speed of hypersonic cruise flight
Fan J(樊菁)
Source PublicationTHEORETICAL & APPLIED MECHANICS LETTERS
2011
Volume1Issue:1Pages:012004
ISSN2095-0349
AbstractA coupling frame of speed gain and maintain was suggested to assess the flight performance of hypersonic cruise vehicles (HCV). The optimal cruise speed was obtained by analyzing the flight performance measured by the ratio of initial boost mass to generalized payload. The performance of HCVs based on rockets and air-breathing ramjets was studied and compared to that of a minimum-energy ballistic trajectory under a certain flight distance. It is concluded that rocket-based HCVs flying at the optimal speed are a very competitive choice at the current stage.
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Language英语
DepartmentLHD微尺度和非平衡流动
Classification二类
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/48735
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
Fan J. Optimal speed of hypersonic cruise flight[J]. THEORETICAL & APPLIED MECHANICS LETTERS,2011,1(1):012004
APA Fan J.(2011).Optimal speed of hypersonic cruise flight.THEORETICAL & APPLIED MECHANICS LETTERS,1(1),012004.
MLA Fan J."Optimal speed of hypersonic cruise flight".THEORETICAL & APPLIED MECHANICS LETTERS 1.1(2011):012004.
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