Flutter analysis of a NACA 64A006 airfoil in small disturbance transonic flow
- 1 April 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (4) , 225-232
- https://doi.org/10.2514/3.44652
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Computation of Unsteady Transonic Flows by the Indicial MethodAIAA Journal, 1978
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977
- The Aeroelastic Analysis of a Two-Dimensional Airfoil in Transonic Flow.Published by Defense Technical Information Center (DTIC) ,1977
- A Comparative Study of Two Computational Methods for Calculating Unsteady Transonic Flows About Oscillating Airfoils.Published by Defense Technical Information Center (DTIC) ,1977
- COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976