Aerodynamic Configuration of the HCW Based on the Lifting Body-Reference-Cited by-同舟云学术

Aerodynamic Configuration of the HCW Based on the Lifting Body

Published:2019-03 Issue:2 Volume:32 Page:04019004
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ma Yang¹,Zhou Wei²,Han Qilong²,Wang Xueren³

Affiliation:

1. Lecturer, Dept. of Missile Engineering, Rocket Force Univ. of Engineering, No. 2 Tongxin Rd., Baqiao District, Xi’an, Shanxi 710025, China (corresponding author).

2. Associate Professor, Dept. of Missile Engineering, Rocket Force Univ. of Engineering, No. 2 Tongxin Rd., Baqiao District, Xi’an, Shanxi 710025, China.

3. Lecturer, Dept. of Missile Engineering, Rocket Force Univ. of Engineering, No. 2 Tongxin Rd., Baqiao District, Xi’an, Shanxi 710025, 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.1943-5525.0000950

Reference21 articles.

1. Characteristics of the AT-303 hypersonic wind tunnel. Part 2. Aerodynamics of the HB-2 reference model

2. Brenda M. K. 2006. “‘Fundamental’ parametric geometry representations for aircraft component shapes.” In Proc. 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conf. Reston VA: American Institute of Aeronautics and Astronautics.

3. Brenda M. K. 2007. “A universal parametric geometry representation method—‘CST.’” In Proc. 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston VA: American Institute of Aeronautics and Astronautics.

4. Comparison of aerodynamic characteristic of near space high lift-drag ratio configuration;Chen B. Y.;Chin. Q. Mech.,2014

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