Subsonic unsteady aerodynamics caused by gusts using the indicial method
- 1 September 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (5) , 869-879
- https://doi.org/10.2514/3.47029
Abstract
No abstract availableKeywords
This publication has 23 references indexed in Scilit:
- Helicopter vibration reduction with trailing edge flapsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- On the Influence of Time‐Varying Flow Velocity on Unsteady AerodynamicsJournal of the American Helicopter Society, 1994
- Indicial lift approximations for two-dimensional subsonic flow as obtained from oscillatory measurementsJournal of Aircraft, 1993
- Calculation of blade-vortex interaction airloads on helicopter rotorsJournal of Aircraft, 1989
- Helicopter impulsive noise: Theoretical and experimental statusJournal of Sound and Vibration, 1986
- Computation of Unsteady Transonic Flows by the Indicial MethodAIAA Journal, 1978
- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971
- Fluctuating Lift Forces on Aerofoils Moving Through Transverse and Chordwise GustsJournal of Basic Engineering, 1968
- The Aerodynamic Force on an Airfoil in a Moving GustJournal of the Aeronautical Sciences, 1956
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938