Study on main flow and fuel injector configurations for Scramjet applications

Author:

Ali Mohammad,Islam A.K.M. Sadrul

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference19 articles.

1. On density effects and large structure in turbulent mixing layer;Brown;J. Fluid Mech.,1974

2. D. Papamoschou, A. Roshko, Observation of Supersonic Free Shear Layers, AIAA Paper, 1986, 86-0162.

3. R.C.A. Rogers, Study of the Mixing of Hydrogen Injected Normal to a Supersonic Airstream, NASA TN, 1971, D-6114.

4. G.O. Kraemer, S.N. Tiwari, Interaction of Two-Dimensional Transverse Jet with a Supersonic Mainstream, NASA CR, 1983, 175446.

5. E.H. Weidner, J.P.A. Drummond, Parametric Study of Staged Fuel Injector Configurations for Scramjet Applications, AIAA Paper, 1981, 81-11468.

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