Design Method of Scramjet Nozzles within Predetermined Geometrical Space and Experimental Verification-Reference-Cited by-同舟云学术

Design Method of Scramjet Nozzles within Predetermined Geometrical Space and Experimental Verification

Published:2022-01 Issue:1 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Chen Yile¹^ORCID,Yu Kaikai²,Song Guangtao³,Ge Jianhui⁴,Xu Jinglei⁵

Affiliation:

1. M.Eng. Candidate, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China. ORCID:

2. Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China (corresponding author).

3. Ph.D. Candidate, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China.

4. Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR China.

5. Professor, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 21006, PR 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.1943-5525.0001372

Reference28 articles.

1. Argrow B. and G. Emanuel. 1989. “A computational analysis of the transonic flow field of two-dimensional minimum length nozzles.” In Proc. 20th Fluid Dynamics Plasma Dynamics and Lasers Conf. New York: American Institute of Aeronautics and Astronautics.

2. Comparison of Minimum Length Nozzles

3. Thrust augmentation optimization through supersonic after-burning in scramjet engine nozzles via surrogate-assisted evolutionary algorithms

4. A new design method on scramjet nozzles with strong geometric constraints;Chen Y.;Acta Aeronaut. Astronaut. Sin.,2020

5. Edwards C. W. Small J. Weidner and P. Johnston. 1975. “Studies of scramjet/airframe integration techniques for hypersonic aircraft.” In Proc. 13th Aerospace Sciences Meeting. New York: American Institute of Aeronautics and Astronautics.

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