NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) Tests of a 10 deg Cone at Mach 1.6
- Author(s):
- Wolf, Stephen W. D. ( MCAT Inst. )
- Laub, James A. ( NASA Ames Research Center )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1997
- Vol.:
- 19970015276
- Issue:
- NASA-TM-110438
- Pt.:
- NAS 1.15:110438
- Page(from):
- 1
- Page(to):
- 28
- Pages:
- 28
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Low-disturbance flow measurements in the NASA-Ames laminar flow supersonic wind tunnel
American Institute of Aeronautics and Astronautics |
7
Technical Paper
WALL ADJUSTMENT STRATEGY SOFTWARE FOR USE WITH THE NASA LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL ADAPTIVE WALL TEST SECTION
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
3
Technical Paper
Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology
National Aeronautics and Space Adminstration |
9
Technical Paper
Mach Number 6 Capability for AEDC Supersonic Wind Tunnel (16S), Requirements and Concepts
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
10
Technical Paper
A Three-Dimensional Orthogonal Laser Velocimeter for the NASA Ames 7- By 10-Foot Wind Tunnel
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
12
Technical Paper
PERFORMANCE TESTS FOR THE NASA AMES RESEARCH CENTER 20 cm X 40cm OSCILLATING FLOW WIND TUNNEL Progress Report.
National Aeronautics and Space Administration |