HELICOPTER BLADE-VORTEX INTERACTION LOCATIONS: SCALE-MODEL ACOUSTICS AND FREE-WAKE ANALYSIS RESULTS
- Author(s):
- Hoad, D. R. ( NASA )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1987
- Issue:
- NASA-TP-2658
- No.:
- H1/02 43813
- Pt.:
- NAS1.60:2658
- Paper no.:
- N87-18537
- Page(from):
- 1
- Page(to):
- 106
- Pages:
- 106
- Pub. info.:
- National Aeronautics and Space Administration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Administration |
7
Technical Paper
On the significance of transonic effects on aerodynamics and acoustics of blade-vortex interaction
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Development of an Indicial Model of Helicopter Tail Rotor Orthogonal Blade Vortex Interaction
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
3
Technical Paper
ROTOR PERFORMANCE CHARACTERISTICS FROM AN AEROACOUSTIC HELICOPTER WING-TUNNEL TEST PROGRAM
National Aeronautics and Space Administration |
9
Technical Paper
Enhancements to a hybrid navier-stokes/free wake method for improved prediction of blade-vortex-interaction phenomena
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
5
Technical Paper
Helicopter rotor tip shapes for reduced blade-vortex interaction - an experiment investigation, part II
American Institute of Aeronautics and Astronautics |
11
Technical Paper
HELICOPTER TAIL ROTOR BLADE-VORTEX INTERACTION NOISE Final Technical Report, 1 Feb. 1986 - 31 Mar. 1987
National Aeronautics and Space Administration |
6
Technical Paper
Investigation of non-linear effects on aerodynamics and acoustics of blade-vortex interactions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |