Stability of Flexible Orthotropic Rectangular Plates in Supersonic Flow: Amplitude-Speed Dependency in Precritical and Postcritical Flight Conditions-Reference-Cited by-同舟云学术

Stability of Flexible Orthotropic Rectangular Plates in Supersonic Flow: Amplitude-Speed Dependency in Precritical and Postcritical Flight Conditions

Author:

Baghdasaryan G. Y.¹,Mikilyan M. A.²,Marzocca P.³

Affiliation:

1. Professor, Institute of Mechanics, National Academy of Sciences of Armenia, Yerevan 0019, Republic of Armenia.

2. Associate Professor, Institute of Mechanics, National Academy of Sciences of Armenia, Yerevan 0019, Republic of Armenia.

3. Associate Professor, Dept. of Mechanical and Aeronautical Engineering, Clarkson Univ., Potsdam, NY 13699 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

Reference22 articles.

2. Ambartsumian S. A. (1974). The general theory of anisotropic shells Nauka Moscow.

3. On the stability of orthotropic plates in supersonic gas flow;Ambartsumian S. A.;Mech. Eng.,1961

5. On stability of orthotropic shells in supersonic gas flow;Baghdasaryan G. Y.;Proc. AS of USSR, Mech. Eng.,1961

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