Study undertaken by Gen Dynamics/Fort Worth to develop inlet and control system for 4 ×24A (J79) engines; concepts proposed were variable afterburner thrust, variable convergent-divergent, nozzle, and variable geometry inlet; tests made and final selection of latter; inlet control, operation and characteristics.
Development of variable geometry inlet for B-58 airplane
SAE -- Paper
SAE Meeting ; 1962 Inlets
1962
7 pages
Aufsatz (Konferenz)
Englisch
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Development of the Variable Geometry Inlet for the B-58 Airplane
SAE Technical Papers | 1962
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