Hypersonic wind tunnels

Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel

R.A. Thompson and Kenneth Sutton.

Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel

Brian R. Hollis.

Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)

A.M. Springer.

A System to measure flow moisture content in hypersonic wind tunnels

James W. West.

Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing

D.E. Reubush, R.L. Puster, H.N. Kelly.

Langley 8-ft. HTT test 139 gas analyses

Danny R. Sprinkle and Patricia P. Davis.

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott D. Holland.

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott D. Holland.

Advanced hypersonic test facilities

edited by Frank Lu, Dan Marren.

On the equilibrium piston technique in gun tunnels

by L. Davies, J. D. Regan and K. A. Dolman.