1.

Technical Paper
Technical Paper
1. Leading edge transition on a 76 degree swept cylinder at Mach 1.6
Coleman, Colin P. ; Poll, D.I.A. ; Laub, James A. ; Wolf, Stephen W.D.
Pub. info.: AIAA paper.  pp.1-12,  1996.  American Institute of Aeronautics and Astronautics
Title of ser.: AIAA Paper : AIAA Fluid Dynamics Conference
Ser. no.: 1996
2.

Technical Paper
Technical Paper
2. Low-disturbance flow measurements in the NASA-Ames laminar flow supersonic wind tunnel
Wolf, Stephen W.D. ; Laub, James A.
Pub. info.: AIAA paper.  pp.1-19,  1996.  American Institute of Aeronautics and Astronautics
Title of ser.: AIAA Paper : AIAA Advanced Measurement and Ground Testing Technology Conference
Ser. no.: 1996
3.

Technical Paper
Technical Paper
3. NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) Tests of a 10 deg Cone at Mach 1.6
Wolf, Stephen W. D. ; Laub, James A.
Pub. info.: NASA Technical Reports.  19970015276  (NASA-TM-110438),  pp.1-28,  1997.  National Aeronautics and Space Adminstration