Jet Engine Inlet Design

References

• Active Control of Boundary-Layer Separation & Flow Distortation in adverse Pressure Gradient Flows via Supersonic Microjets, proposal to NASA Langley Research Center, Farrukh Alvi

•http://www.desktopaero.com/appliedaero/blayers/blayers.html

•http://www.aircraftenginedesign.com/abefs.html

•Alvi, Elavarasan, Shih, Garg, and Krothapalli, “Active control of Supersonic Impingin Jets using Micro Jets, AIAA 2000-2236, submitted to AIAA Journal

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