Airframe installation effects at transonic speeds on underwing supersonic cruise exhaust nozzles, using flight and wind tunnel tests
Flight and wind tunnel investigation of installation effects on underwing supersonic cruise exhaust nozzles at transonic speeds
NATO, AGARD, AERODYNAMIC INTERFERENCE SPECIALISTS MEETING ; 1970 ; SILVER SPRING, MD
01.09.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch