Numerical study of aerodynamic characteristics of FSW aircraft with different wing positions under supersonic condition

Author:

Lei Juanmian,Zhao Shuai,Wang Suozhu

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference15 articles.

1. Behrbohm H. Basic low speed aerodynamic of short-coupled canard configuration of small aspect ratio. Sweden: Linkoping; 1965. Report No.: SAABTN-60.

2. Vortical flowfield structure at forward swept-wing configurations;Breitsamter;J Aircr,2001

3. Aerodynamic characteristics of canard-forward sweptwing aircraft configurations;Zhang;J Aircr,2013

4. Investigation of vortex interaction in canard-FSW configurations based on the numerical wind tunnel method;Zhang;Chin J Aeronaut,2009

5. Stability and control of a three-surface, FSW configuration;Owens;J Aircr,1996

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