Combustion Wind Tunnels

12 books
Finite-rate water condensation in combustion-heated wind tunnelsWayne D. Erickson
⏱ 1h 9m

Finite-rate water condensation in combustion-heated wind tunnels

Wayne D. Erickson

198869 pp.
Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulationLawrence D. Huebner
⏱ 46m

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation

Lawrence D. Huebner

199346 pp.
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott Douglas Holland

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

Scott Douglas Holland

1994No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott D. Holland

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

Scott D. Holland

1994No page data
Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinderDale A. Babcock

Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinder

Dale A. Babcock

1997No page data
Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facilityJose Tamagno
⏱ 10m

Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility

Jose Tamagno

199010 pp.
Investigation of ramp injectors for supersonic mixing enhancementY. Haimovitch

Investigation of ramp injectors for supersonic mixing enhancement

Y. Haimovitch

1994No page data
Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8Unknown Author

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8

Unknown Author

2000No page data
Shock-tunnel combustor testing for hypersonic vehiclesMark Loomis

Shock-tunnel combustor testing for hypersonic vehicles

Mark Loomis

1994No page data
NASA's hypersonic research engine projectEarl H. Andrews

NASA's hypersonic research engine project

Earl H. Andrews

1994No page data
Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10Scott Douglas Holland

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10

Scott Douglas Holland

1995No page data
Mach 10 experimental database of a three-dimensional scramjet inlet flow fieldScott D. Holland
⏱ 3h 34m

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

Scott D. Holland

1995214 pp.