Blank Cover Image

HIGHLIGHTS OF EXPERIENCE WITH A FLEXIBLE WALLED TEST SECTION IN THE NASA LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Author(s):
Wolf, Stephon W.D. et al. ( Vigyan Research Associates, Inc., Hampton, Va. / NASA )  
Publication title:
NASA Technical Reports(N89)
Pub. Year:
1988
Issue:
NASA-TM-101491
No.:
G3/09 0167512
Pt.:
NAS1.15:101491
Paper no.:
N89-10060
Page(from):
1
Page(to):
12
Pages:
12
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper WALL ADJUSTMENT STRATEGY SOFTWARE FOR USE WITH THE NASA LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL ADAPTIVE WALL TEST SECTION

Wolf, Stephen W.D.

National Aeronautics and Space Administration
7 Technical Paper A Study of Juncture Flow in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel

Chokani, Ndaona, Dr., Milholen, William E., II

National Aeronautics and Space Adminstration
2 Technical Paper Calibration of the 13- by 13-Inch Adaptive Wall Test Section for the Langley 0.3-Meter Transonic Cryogenic Tunnel

Mineck, Raymond E., Hill, Acquilla S.

National Aeronautics and Space Adminstration
8 Technical Paper HIGH REYNOLDS NUMBER TRANSONIC TESTS ON A NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Ladson, Charies L. et al.

National Aeronautics and Space Administration
3 Technical Paper HARDWARE AND OPERATING FEATURES OF THE ADAPTIVE WALL TEST SECTION FOR THE 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Mineck, Raymond E.

National Aeronautics and Space Administration
9 Technical Paper STUDIES OF CONDENSATION EFFECTS ON AIRFOIL TESTING IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Hall, R.M.

National Aeronautics and Space Administration
4 Technical Paper HIGH REYNOLDS NUMBER TESTS OF THE NASA SC (2) -0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Mineck, E.

National Aeronautics and Space Administration
10 Technical Paper HIGH REYNOLDS NUMBER TESTS OF A DOUGLAS DLBA 032 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Johnson, Charies B. et al.

National Aeronautics and Space Administration
5 Technical Paper AERODYNAMIC PERFORMANCE AND PRESSURE DISTRIBUTIONS FOR A NASA SC(2)-0714 AIRFOIL TESTED IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Jenkins, Renaldo V. et al.

National Aeronautics and Space Administration
11 Technical Paper IMPROVEMENT IN THE QUALITY OF FLOW VISUALIZATION IN THE LANGLEY 0.3.METER TRANSONIC CRYOGENIC TUNNEL

Snow, W.L.

National Aeronautics and Space Administration
6 Technical Paper Performance of TWNTN4A Correction Code at the 0.3-Meter Transonic Cryogenic Tunnel at NASA Langley

Ghosh, A., Machida, R., Everhart, J.

American Institute of Aeronautics and Astronautics
12 Technical Paper NASA SC(2)-0714 AIRFOIL DATE CORRECTED FOR SIDEWALL BOUNDARY-LAYER EFFECTS IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Jenkins, Renaldo V.

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