Double Swept Waverider from Osculating-Cone Method-Reference-Cited by-同舟云学术

Double Swept Waverider from Osculating-Cone Method

Published:2018-11 Issue:6 Volume:31 Page:06018004
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Chuanzhen¹,Bai Peng²,Yang Yunjun³,Zhou Weijiang³

Affiliation:

1. Ph.D. Student, Dept. of Theoretical and Applied Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing 100074, China.

2. Professor, Dept. of Theoretical and Applied Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing 100074, China (corresponding author).

3. Professor, Dept. of Theoretical and Applied Aerodynamics, China Academy of Aerospace Aerodynamics, Beijing 100074, 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.1943-5525.0000918

Reference15 articles.

1. Bowcutt K. G. 1986. “Optimization of hypersonic waveriders derived from cone flows including viscous effects.” Ph.D. dissertation Dept. of Aerospace Engineering Univ. of Maryland.

2. Research on the methods of generation and design of osculating cone waverider with constant angle of sweepback;Duan Y. H.;Acta Aeronout. et Astronaut. Sin.,2016

3. Longitudinal static stability analysis of hypersonic waveriders;Jia Z. A.;Sci. China Ser. E- Tech.,2014

4. A method for designing lifting configurations for high supersonic speeds using axisymmetric flow field;Jones J. G.;Circ. Arch. Appl. Mech.,1968

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