Performance of Three Isentropic All Internal Compression Axisymmetric Inlets Designed for Mach 2.5
1960
29 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Air jet , Compression tube , Performance characteristics , Air , Angle of attack , Axisymmetry , Bleed , Change , Characteristics , Compression , Inlet , Internal , Isentropy , Jet , Mach number , Optimum , Performance , Speed , Starting , Supersonic , System , Tolerance , Tube