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

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

By C. Y. Tsai

Air-breathing aerospace plane development essential

By Unmeel B. Mehta

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

By D. W. Riggins

Shock-tunnel combustor testing for hypersonic vehicles

By Mark Loomis

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

By Tawit Chitsomboon

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

By Alexander S. Roudakov

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

By Mark D. Ardema

Investigation of ramp injectors for supersonic mixing enhancement

By Y. Haimovitch

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

By Scott Douglas Holland

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

By Scott D. Holland

Instrumentation development for study of Reynolds analogy in reacting flows

By Dianne J. DeTurris

Hypersonic combined cycle propulsion

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

Viscous computations of cold air/airflow around scramjet nozzle afterbody

By Oktay Baysal

A first scramjet study

By George Emmanuel

An investigation of a contoured wall injector for hypervelocity mixing augmentation

By Ian A. Waitz

An outlook on hypersonic flight

By Griffin Y. Anderson

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

By R. Skyring

Measured operating characteristics of a rectangular combustor/inlet isolator

By David A. Bement

A numerical and experimental study of a supersonic combustor employing swept ramp fuel injectors

By Dean R. Eklund

Supersonic reacting internal flow fields

By J. Philip Drummond

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

By Scott D. Holland

Shock tunnel studies of scramjet phenomena

By

Turbulent transport models for scramjet flowfields

By M. M. Sindir