Multiobjective Optimization of Scramjet Strut Geometry Using Computational Fluid Dynamics Approach-Reference-Cited by-同舟云学术

Multiobjective Optimization of Scramjet Strut Geometry Using Computational Fluid Dynamics Approach

Published:2024-07 Issue:4 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Pirkandi Jamasb¹^ORCID,Hashemabadi Mahdi²,Zakeri Mahnaz³^ORCID

Affiliation:

1. Associate Professor, Faculty of Aerospace, Malek-Ashtar Univ. of Technology, Tehran 1774-15875, Iran (corresponding author). ORCID: .

2. Assistant Professor, Faculty of Aerospace, Malek-Ashtar Univ. of Technology, Tehran 1774-15875, Iran.

3. Associate Professor, Advanced Structures Research Laboratory, Faculty of Aerospace Engineering, K. N. Toosi Univ. of Technology, Tehran 16569-83911, Iran. ORCID:

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4885

Reference49 articles.

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2. Numerical assessment of ejector operation for refrigeration applications based on CFD

3. LES of supersonic combustion in a scramjet engine model

4. Boyce R. S. Gerard and A. Paull. 2003. “The HyShot scramjet flight experiment-flight data and CFD calculations compared.” In Proc. 12th AIAA Int. Space Planes and Hypersonic Systems and Technologies 7029. Reston VA: American Institute of Aeronautics and Astronautics.

5. Comparison of Supersonic Combustion Between Impulse and Vitiation-Heated Facilities