Some measured and calculated effects of a tip vortex modification device on impulsive noise
- 16 August 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Some results of the testing of a full-scale Ogee tip helicopter rotor; acoustics, loads, and performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Development of an Improved Design Tool for Predicting and Simulating Helicopter Rotor NoisePublished by Defense Technical Information Center (DTIC) ,1974
- Vortex Modification by Mass Injection and by Tip Geometry VariationPublished by Defense Technical Information Center (DTIC) ,1973
- An investigation of impulsive rotor noise of a model rotorJournal of Sound and Vibration, 1973
- STUDY OF MODIFICATION OF ROTOR TIP VORTEX BY AERODYNAMIC MEANSPublished by Defense Technical Information Center (DTIC) ,1970