Computational aerodynamic optimization of wing-design concept at supersonic conditions by means of the response surface method
Crossref DOI link: https://doi.org/10.1007/s40430-018-1150-4
Published Online: 2018-04-23
Published Print: 2018-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Manshadi, Mojtaba Dehghan
Aghajanian, Soheil
Funding for this research was provided by:
Malek Ashtar University of Technology
Text and Data Mining valid from 2018-04-23
Article History
Received: 25 June 2017
Accepted: 22 March 2018
First Online: 23 April 2018