An investigation of counterrotating tip vortex interaction
- Author(s):
- Majjigi, R. K. ( General Electric Co. )
- Uenishi, K. ( General Electric Co. )
- Gliebe, P. R. ( General Electric Co. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1989
- Issue:
- NASA-CR-185135
- Pt.:
- NAS 1.26:185135
- Paper no.:
- N90-11549
- Page(from):
- 1
- Page(to):
- 124
- Pages:
- 124
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
DEVELOPMENT OF A ROTOR WAKE/VORTEX MODEL. VOLUME 2: USER'S MANUAL FOR COMPUTER PROGRAM Final Report
National Aeronautics and Space Administration |
7
Technical Paper
Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems
National Aeronautics and Space Adminstration |
2
Technical Paper
Experimental Investigation of Shock-Cell Noise Reduction for Dual-Stream Nozzles in Simulated Flight
National Aeronautics and Space Administration |
Society of Automotive Engineers |
3
Technical Paper
Helicopter rotor tip shapes for reduced blade-vortex interaction - an experiment investigation, part II
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
4
Technical Paper
Periodical Unsteady Flow within a Rotor Blade Row of an Axial Compressor: Part II - Wake-Tip Clearance Vortex Interaction.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Axial core flow effects on the interaction of a rotor-tip vortex with an airframe
American Institute of Aeronautics and Astronautics |