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by Tom Norman
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Non-coalescence effects in microgravity
G. Paul Neitzel
Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Emma Jean Landrum
Pockels-effect cell for gas-flow simulation
David Weimer
Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Experimental Hydraulics : Methods, Instrumentation, Data Processing and Management : Volume II
Jochen Aberle
In-flight flow visualization results from the X-29A aircraft at high angles of attack
John H. Del Frate
Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
Steven A. Johnson
Computer simulation of shaped charge problems
Wen Ho Lee
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
P. S. Barna
In-flight flow visualization using infrared thermography
C. P. Van Dam
