Novel Osculating Flowfield Methodology for Hypersonic Waverider Vehicles Based on Variable Shock Angle-Reference-Cited by-同舟云学术

Novel Osculating Flowfield Methodology for Hypersonic Waverider Vehicles Based on Variable Shock Angle

Published:2018-07 Issue:4 Volume:31 Page:04018043
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Zhen¹,Liu Jun²,Ding Feng³,Li Kai⁴,Xia Zhixun²

Affiliation:

1. Ph.D. Student, Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha, Hunan 410073, People’s Republic of China (corresponding author).

2. Professor, Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha, Hunan 410073, People’s Republic of China.

3. Lecturer, Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha, Hunan 410073, People’s Republic of China.

4. Ph.D. Student, Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha, Hunan 410073, People’s Republic of China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000864

Reference28 articles.

1. Hypersonic and High-Temperature Gas Dynamics, Second Edition

2. Bowcutt K. G. J. D. Anderson and D. Capriotti. 1987. “Viscous optimized hypersonic waveriders.” In Proc. 25th AIAA Aerospace Sciences Meeting. Reno NV: American Institute of Aeronautics and Astronautics.

3. Center K. B. H. Sobieczky and F. C. Dougherty. 1991. “Interactive design of hypersonic waverider geometrics.” In Proc. 22nd Fluid Dynamics Plasma Dynamics and Lasers Conf. Honolulu HI.

4. Bluntness impact on performance of waverider

5. Corda S. and J. D. Anderson. 1988. “Viscous optimized hypersonic waveriders designed from axisymmetric flow fields.” In Proc. 26th Aerospace Sciences Meeting. Reno NV: American Institute of Aeronautics and Astronautics.

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