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Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports
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Ranard, E. and Davison, B., "Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports," SAE Technical Paper 610097, 1961, https://doi.org/10.4271/610097.Also In
References
- Flanders T. A. “Control of Supersonic Inlets.” Presented at the Aviation Conference, Los Angeles, California, ASME, March 12-16” 1961
- Barry F. W. “Transient Shock Motion in a Supersonic Diffuser Having a Variable Bypass.” UAC Research Department Report R-0925-4 May 26 1959
- Hurrell H. G. “Analysis of Shock Motion in Ducts During Disturbances in Downstream Pressure.” NACA Technical Note 4090 September 1957
- Fraiser H. R. “Supersonic Inlet Dynamics.” Journal of Aero/Space Sciences 27 6 June 1960
- Thayler G. Brown R. G. “Analysis and Design of Feedback Control Systems.” McGraw-Hill
- Sens W. H. Slaiby T. G. “A Consideration of Powerplants for Supersonic Transport Aircraft.” Presented at the SAE National Aeronautic Meeting New York, N. Y. April 4-7 1961