Blank Cover Image

Results of Tests Performed on the Acoustic Quiet Flow Facility Three-Dimensional Model Tunnel

Author(s):
Barna, P. S. ( Lockheed Engineering and Sciences Co. )  
Publication title:
NASA Technical Reports
Pub. Year:
1995
Vol.:
19960047449
Issue:
NASA-CR-198311
Pt.:
NAS 1.26:198311
Page(from):
1
Page(to):
38
Pages:
38
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper Results of tests performed on the Acoustic Quiet Flow Facility Three-Dimensional Model Tunnel: Report on the Modified D.S.M.A. Design

Barna, P. S.

National Aeronautics and Space Adminstration
7 Technical Paper Flow Visualization Measurement Techniques for High-Speed Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel

Matsumura, S., Schneider, S.P., Berry, S.A.

American Institute of Aeronautics and Astronautics
2 Technical Paper Modelling of natural transition in properly three-dimensional flows

Arthur, M. T., Horton, H. P., Mughal, M. S.

American Institute of Aeronautics and Astronautics
8 Technical Paper Three-dimensional aerodynamic analysis of a subsonic transport high-lift configuration and comparisons with wind-tunnel test results

Edge, D. Christian, Perkins, John N.

National Aeronautics and Space Adminstration
3 Technical Paper Studies of small-scale low-speed wind tunnel configurations

Barna, P.S.

American Institute of Aeronautics and Astronautics
9 Technical Paper The Effects of Test Scale and Facility Details on the Flow Field Features of Supersonic Three-Dimensional Fin/ Plate Interactions.

Neumann, R.K., Hayes, J.R.

American Institute of Aeronautics and Astronautics
4 Technical Paper Inlet Flow Test Calibration for a Small Axial Compressor Facility Part 1-Design and Experimental Results

Miller, D.P., Prahst, P.S.

National Aeronautics and Space Adminstration
10 Technical Paper Wind Tunnel Test of a Three-Element Airfoil Configuration: Development of Experimental Apparatus and Procedure for Obtaining Reliable Results

R. Girardi, M. Assato, P. Komatsu, N. Fico

American Institute of Aeronautics and Astronautics
5 Technical Paper Effect of Collector Configuration on Test-Section Turbulence Levels in an Open-Jet Wind Tunnel

Manuel, G.S., Molloy, John K., Barna, P.S.

National Aeronautics and Space Adminstration
11 Technical Paper Acoustic wave propagation in two dimensional sheared ducted flows

Longatte, E., Lafon, P., Candel, S.

American Institute of Aeronautics and Astronautics
6 Technical Paper The Driveability Test Facility Wind Tunnel No. 8.

Walter, J., Duell, E., Martindale, B., Arnette, S., Nagle, P.A.

Society of Automotive Engineers
12 Technical Paper The NASA Langley 16-foot Transonic Tunnel: Historical overview, facility description, calibration, flow characteristics, and test capabilities

Capone, Francis J., Bangert, Linda S., Asbury, Scott C., Mills, Charles T. L., Bare, E. Ann

National Aeronautics and Space Adminstration
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12