Probing Real Gas and Leading-Edge Bluntness Effects on Shock Wave Boundary-Layer Interaction at Hypersonic Speeds-Reference-Cited by-同舟云学术

Probing Real Gas and Leading-Edge Bluntness Effects on Shock Wave Boundary-Layer Interaction at Hypersonic Speeds

Published:2019-11 Issue:6 Volume:32 Page:04019089
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Desai Siddesh¹,Brahmachary Shuvayan¹,Gadgil Hrishikesh²,Kulkarni Vinayak³

Affiliation:

1. Research Scholar, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India.

2. Assistant Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, Maharashtra 400076, India.

3. Associate Professor, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India (corresponding author).

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.1943-5525.0001085

Reference33 articles.

1. Comparative performance assessments of surface junction probes for stagnation heat flux estimation in a hypersonic shock tunnel

2. Brahmachary S. G. Natarajan V. Kulkarni N. Sahoo and S. R. Nanda. 2017. Application of greedy and heuristic algorithm based optimisation methods towards aerodynamic shape optimization. In Vol. 1 of Proc. 7th Int. Conf. on Soft Computing for Problem Solving 937–948. Bhubaneswar India: Indian Institute of Technology Bhubaneswar.

3. Finite-volume method for the calculation of compressible chemically reacting flows

4. A Fast Elitist Non-dominated Sorting Genetic Algorithm for Multi-objective Optimization: NSGA-II

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