Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
- Author(s):
- Devenport, William J. ( Virginia Polytechnic Inst. )
- Glegg, Stewart A. L. ( Florida Atlantic Univ. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1995
- Issue:
- NASA-CR-198590
- Pt.:
- NAS 1.26:198590
- Paper no.:
- N95-28193
- Page(from):
- 1
- Page(to):
- 53
- Pages:
- 53
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Flow Structure Generated by Perpendicular Blade Vortex Interaction and Implications for Helicopter Noise Predictions
National Aeronautics and Space Adminstration |
7
Technical Paper
Wavenumber frequency spectra of turbulence in a lifting wake for broadband noise prediction
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Flow structure generated by perpendicular blade-vortex interaction and implications for helicopter noise prediction.
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
9
Technical Paper
The Spectral and Statistical Properties of Turbulence Generated by a Vortex/Blade-Tip Interaction
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
VELOCITY MEASUREMENTS IN A TURBULENT TRAILING VORTEX AND THEIR APPLICATION TO BWI NOISE FREDICTION
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |