Refined Prediction Method for Supersonic Nonsteady Aerodynamics with AIC Partition Scheme
- 1 August 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (8) , 609-617
- https://doi.org/10.2514/3.57536
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- An Improved Mach-Box Approach for Supersonic Oscillatory PressuresJournal of Aircraft, 1977
- Unsteady Aerodynamics of Nonplanar Wings and Wing-Tail Configurations of Elastic Flight Vehicles in Supersonic FlightJournal of Aircraft, 1973
- A Refined Prediction Method for the Unsteady Aerodynamics of Supersonic Elastic AircraftJournal of Aircraft, 1972
- Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic EdgesJournal of the Aeronautical Sciences, 1955