Review of rotary-wing V/STOL dynamic and aeroelastic problems
- 17 February 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐RotorsJournal of the American Helicopter Society, 1967
- Torsional oscillation of helicopter blades due to stall.Journal of Aircraft, 1966
- The Use of an Analogue Computer to Calculate Rotor Blade MotionJournal of the American Helicopter Society, 1964
- An Experimental Investigation of Stall FlutterJournal of the American Helicopter Society, 1962
- Recent Studies of the Pitch‐Lag Instabilities of Articulated RotorsJournal of the American Helicopter Society, 1961
- Some Aeroelastic Problems of Tilt‐Wing; VTOL AircraftJournal of the American Helicopter Society, 1958
- Investigation of Helicopter Blade Flutter and Load Amplification ProblemsJournal of the American Helicopter Society, 1957
- A Two-Dimensional Approximation to the Unsteady Aerodynamics of Rotary WingsJournal of the Aeronautical Sciences, 1957
- Stability of a Flexible Helicopter Rotor Blade in Forward FlightJournal of the Aeronautical Sciences, 1956
- Helicopter Blade Vibration and FlutterJournal of the American Helicopter Society, 1956