Calculation of transonic steady and oscillatory pressures on a low aspect ratio model
- 1 June 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (6) , 392-398
- https://doi.org/10.2514/3.45458
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Transonic calculations for a flexible supercritical wing and comparison with experimentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control surfacePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Non-isentropic unsteady transonic small disturbance theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Efficient algorithm for unsteady transonic aerodynamics of low-aspect-ratio wingsJournal of Aircraft, 1985
- Effects of viscosity on transonic-aerodynamic and aeroelastic characteristics of oscillating airfoilsJournal of Aircraft, 1984
- Transonic pressure distributions on a rectangular supercritical wingoscillating in pitchJournal of Aircraft, 1984
- An algorithm for unsteady transonic flow about tapered wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- The LANN program - An experimental and theoretical study of steady and unsteady transonic airloads on a supercritical wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Static and unsteady pressure measurements on a 50 degree clipped delta wing at M = 0.9Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Transonic Unsteady Airloads on an Energy Efficient Transport Wing with Oscillating Control SurfacesJournal of Aircraft, 1981