Computational aerodynamic optimization of wing-design concept at supersonic conditions by means of the response surface method-Reference-Cited by-同舟云学术

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Computational aerodynamic optimization of wing-design concept at supersonic conditions by means of the response surface method

Published:2018-04-23 Issue:5 Volume:40 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Manshadi Mojtaba Dehghan,Aghajanian Soheil

Funder

Malek Ashtar University of Technology

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

http://link.springer.com/article/10.1007/s40430-018-1150-4/fulltext.html

Reference46 articles.

1. Anderson JD (1997) A history of aerodynamics and its impact on flying machines. Cambridge University Press, Cambridge

2. Secanell M, Suleman A, Gamboa P (2006) Design of a morphing airfoil using aerodynamic shape optimization. AIAA J 44:1550–1562. https://doi.org/10.2514/1.18109

3. Lock RC, Bridgewater J (1967) Theory of aerodynamic design for swept-winged aircraft at transonic and supersonic speeds. Prog Aerosp Sci 8:139–228. https://doi.org/10.1016/0376-0421(67)90004-8

4. Sadraey M (2012) Aircraft design: a systems engineering approach. Wiley, Amsterdam

5. Talay TA (2012) Introduction to the aerodynamics of flight. NASA, New York

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