Numerical analysis on flutter of Busemann-type supersonic biplane airfoil

Author:

Zhou Hao,Wang Gang,Liu Zhikan

Funder

Northwestern Polytechnical University, PR China

National Natural Science Foundation of China

“111” Project of China

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference56 articles.

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2. Low-Boom/Low-Drag Design optimization of innovative supersonic transport configuration;Ban;J. Aircr.,2017

3. Role of shocks in transonic/supersonic compressor rotor flutter;Bendiksen;AIAA J.,1986

4. The divergence of supersonic wings including chordwise bending;Biot;J. Aeronaut. Sci.,1956

5. Computational Fluid Dynamics: Principles and Applications;Blazek,2005

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