A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft

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 ̊

Emma Jean Landrum

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