Romance · 1992 · unrated
Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities
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Explicit
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2
March to the Grave
Have baby, need billionaire
Collided
