Results of analytical and design studies are presented for a water-glycol convective cooling system for the airframe structure of a hypersonic transport. System configurations and weights are compared. The influences of system pressure drop and flow control schedules on system weight are defined. (Author)
Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe
1971
131 pages
Report
Keine Angabe
Englisch