The Measurement of Disturbance Levels in the Langley Research Center 20-inch Mach 6 Tunnel
- Author(s):
- Stainback, P.C. ( Analytical Services and Materials, Inc. )
- Kubendran, L.R.
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1994
- Issue:
- NASA-CR-4571
- Pt.:
- NAS 1.26:4571
- Paper no.:
- N94-26548
- Page(from):
- 1
- Page(to):
- 23
- Pages:
- 23
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Adminstration |
7
Technical Paper
Boundary Layer Stability Calculations of the HIFiRE Flight 1 Vehicle in the LaRC 20-Inch Mach 6 Air Tunnel
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
8
Technical Paper
USER GUIDE FOR THE DIGITAL GONTROL SYSTEM OF THE NASA/LANGLEY RESEARCH CENTER'S 13-INCH MAGNETIC SUSPENSION AND
National Aeronautics and Space Administration |
3
Technical Paper
Disturbance-Level and Transition Measurements in a Conical Boundary Layer at Mach 6
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0.0362-Scale X-38 (Rev. 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
10
Technical Paper
Aerothermodynamic Testing of the Crew Exploration Vehicle in the LaRC 20-Inch Mach 6 and 31-Inch Mach 10 Tunnels
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6wind Tunnels.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |