Contents: GENERAL DESCRIPTION; DEFINITION OF THE X 81 COMBINED ENGINE; PERFORMANCE CHARACTERISTICS--Sea level static; flight air mass flow; flight without afterburning; flight with afterburning; Influence of the air inlet total pressure recovery; Influence of the nozzle thrust coefficient; Influence of air bleed; OVERALL DIMENSIONS - WEIGHT; INSTALLATION - HANDLING; AND COMBUSTION TESTS.
Experimental and Design Studies for Turbo-Ramjet Combination Engine. Volume 1 - Specifications and Performance
1966
68 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Turboramjet engines , Specifications , Performance(Engineering) , Turbofan engines , Combustion chambers , Turbojet exhaust nozzles , Afterburners , Control systems , Gas flow , Fuel consumption , Altitude , Pressure , Recovery , Weight , Combustion , Secondary flow , Thrust , Bleed systems , Mounting brackets , Handling , Ducts , Jet engine inlets , France , Tf-106 engines
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