Explore Books on
supersonic combustion ramjet engines

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

By Lawrence D. Huebner

Air-breathing aerospace plane development essential

By Unmeel B. Mehta

A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE

By C. Y. Tsai

Shock-tunnel combustor testing for hypersonic vehicles

By Mark Loomis

High-speed engine/component performance assessment using exergy and thrust-based methods

By D. W. Riggins

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

By Mark D. Ardema

Viscous computations of cold air/airflow around scramjet nozzle afterbody

By Oktay Baysal

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

By Scott Douglas Holland

A first scramjet study

By George Emmanuel

Instrumentation development for study of Reynolds analogy in reacting flows

By Dianne J. DeTurris

Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations

By Tawit Chitsomboon

Investigation of ramp injectors for supersonic mixing enhancement

By Y. Haimovitch

Hypersonic combined cycle propulsion

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

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

By Scott D. Holland

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program

By Alexander S. Roudakov

Flow establishment in a generic scramjet combustor

By P. A. Jacobs

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

By Thomas A. Edwards

An investigation of a contoured wall injector for hypervelocity mixing augmentation

By Ian A. Waitz

A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field

By Scott Douglas Holland

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

By Scott Douglas Holland

Mach 10 computational study of a three-dimensional scramjet inlet flow field

By Scott Douglas Holland

Scramjet mixing establishment times for a pulse facility

By R. Clayton Rogers

Progress toward synergistic hypermixing nozzles

By D. O. Davis

Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system

By Nicholas J. Georgiadis