Aerodynamic and Hydrodynamic Characteristics of a Deck-inlet Multijet Water-based-aircraft Configuration Designed for Supersonic Flight
1956
From Introduction: "In the present investigation, lift, drag, and pitching moment were determined over a Mach number range 0.6 to 1.42. Smooth-water takeoff and landing stability and resistance were investigated. A brief check of the rough-water spray and behavior was also made."
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