Discover Supersonic Combustion Ramjet Engines

Shock-tunnel combustor testing for hypersonic vehicles

Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems

Reduced H2-O2 mechanisms for use in reacting flow simulation

Supersonic combustion ramjet research at Langley

Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4

Precombustion shock structure in scramjet engines

Calculated chemical and vibrational nonequilibrium effects in NASP-type nozzles

Shock tunnel studies of scramjet phenomena

Research in robust control for hypersonic vehicles

A mixing augmentation technique for hypervelocity scramjets

The effect of exhaust plume/afterbody interaction on installed scramjet performance

Scramjet testing from Mach 4 to 20

Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion

Instrumentation development for study of Reynolds analogy in reacting flows

Hypersonic combined cycle propulsion

Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K

Computational analysis of the combustion process in an axisymmetric RBCC flowpath

Heat pipe cooling for scramjet engines

Experimental determination of hydrogen-air detonation pressure limit and scramjet application

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

Studies in scramjet flowfields

Mixing enhancement of reacting parallel fuel jets in a supersonic combustor

An outlook on hypersonic flight

Viscous computations of cold air/airflow around scramjet nozzle afterbody