Low-Speed Wind-Tunnel Test of an Unpowered High-Speed Stoppable Rotor Concept in Fixed-Wing Mode
- Author(s):
- Lance, Michael B. ( Lockheed Engineering & Sciences Company )
- Sung, Daniel Y. ( Sterling Software )
- Stroub, Robert H. ( Ames Research Center )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1991
- Issue:
- NASA-TM-4250
- No.:
- H1/02 0319917
- Pt.:
- NAS 1.15:4250
- Paper no.:
- N91-18033
- Page(from):
- 1
- Page(to):
- 53
- Pages:
- 53
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Administration |
7
Technical Paper
LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 1: TEST
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
8
Technical Paper
LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 2: TEST DATA
National Aeronautics and Space Administration |
3
Technical Paper
An experimental investigation of helicopter rotor hub fairing drag characteristics
National Aeronautics and Space Adminstration |
Society of Automotive Engineers |
4
Technical Paper
A Comparative Assessment of High Speed Rotorcraft Concepts (HSRC): Reaction Driven Stopped Rotor/Wing Versus Variable Diameter Tiltrotor
Society of Automotive Engineers |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |