Current position: Home >> Scientific Research >> Paper Publications

Thermal-Aeroelastic Investigation of a Hypersonic Panel Vibration Based on a Developed MMC Method

Release Time:2024-08-30  Hits:

Indexed by: Journal Papers

Document Code: 390657

Date of Publication: 2024-03-10

Journal: AEROSPACE

Volume: 11

Issue: 3

Key Words: FLUTTER; HARMONIC GRADIENT-METHOD; TOPOLOGY OPTIMIZATION

Prev One:Numerical aerodynamic analysis of bluff bodies at a high Reynolds number with three-dimensional CFD modeling

Next One:Numerical studies on the thermal-fluid-structure coupling analysis method of hypersonic flight vehicle
Recommended Ph.D.Supervisor Recommended MA Supervisor Institutional Repository Personal Page

Address: No.2 Linggong Road, Ganjingzi District, Dalian City, Liaoning Province, P.R.C., 116024

Click:Times MOBILE Version
The Founding Time : ..
The Last Update Time : ..

Browse on mobile