LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 1: TEST
- Author(s):
- Stewart, V.R. ( Rockwell International Corp. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1987
- Issue:
- NASA-CR-178348
- No.:
- G3/02 0097190
- Pt.:
- NAS1.26:178348
- Paper no.:
- N87-27641
- Page(from):
- 1
- Page(to):
- 96
- Pages:
- 96
- Pub. info.:
- National Aeronautics and Space Administration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
1
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 |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
8
Technical Paper
PROPULSION AND AIRFRAME AERODYNAMIC INTERACTIONS OF SUPERSONIC V/STOL CONFIGURATIONS. VOLUME 2: WIND TUNNEL TEST FORCE AND MOMENT DATA REPORT
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A WING-CANARD CONFIGURATION WITH UNDERWING SPANWISE BLOWING ON THE
National Aeronautics and Space Administration |
6
Technical Paper
Low-Speed Wind-Tunnel Test of an Unpowered High-Speed Stoppable Rotor Concept in Fixed-Wing Mode
National Aeronautics and Space Adminstration |
12
Technical Paper
A Low-Speed Wind Tunnel Study of Vortex Interation Control techniqus on a Chine-Forebody/Delta-Wing Configuration
National Aeronautics and Space Adminstration |