1. signof aVery-Low-BleedMach2.5Mixed-CompressionInletwith 45PercentInternalContraction.NASA TMX-3135,1975. 2.Neumann.H. E.;Wasserbauer,J.E: andShaw,R. I.:Per
2. formanceof VortexGeneratorsinaMach2.5Low-BleedFull-Scale 45-Percent-Internal-ContractionAxisymmetricInlet.NASATMX-3195,1975. 3.Wasserbauer,J.E;Neumann,H.E.: andShaw,R.J.: Dis
3. tortioninaFull-ScaleBiconeInletwith 45Perccntln-ternalContraction.NASA TMX-3133,1975. W 4.Wasserbauer.J. E;Neumann,H. E.: andShaw,R.I.:Per
4. formance andSurgeLimitsofaTF30-P-3Turbofan Engine/AxisymmeUicMixed-CompressionInletPropulsionSystematMach2.5.NASATF-2.161, 1985. S.Anderson,B. H.: DesignofSupersonicInletsbyaCom
5. puterProgramIncorporatingtheMethodofCharacteristics.NASATN-D4960,1969. 6.Bowditch,D.N.: SomeDesignConsiderationsforSuper