Contents: Configuration Design and Development -- Landing gear study, Body depth study, Vertical tail studies, Weight review, Interior arrangement development, and Landing gear deflection systems; Performance -- Wind tunnel testing, Performance analysis, Stability and control, Flight dynamics, Noise, and Airport compatibility; Structures -- Criteria and loads analysis, Stress analysis, Structural design, Flutter and dynamic loads analysis, Weight and balance analysis, and Structural and material tests; Propulsion -- Inlet and exhaust test and analysis, Engine performance analysis, Propulsion system integration, Fuel system, and Propulsion control; Systems -- Avionics, Flight controls, Hydraulics and electrical, Environmental control and oxygen systems, Fire detecting and extinguishing systems, Flight instrument systems, Accessory power drive system; and Design Support and Integration -- Maintainability engineering and Customer engineering.
Supersonic Transport Program. Phase Iib
1965
167 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Supersonic aircraft , Jet transport planes , Design , Tails(Aircraft) , Aerodynamic configurations , Airplane models , Model tests , Wind tunnel models , Titanium alloys , Structures , Fracture(Mechanics) , Toughness , Landing gear , Performance(Engineering) , Systems engineering , Research management , Supersonic transports
Supersonic Transport Program. Phase Iib
NTIS | 1965
Supersonic Transport Program. Phase Iib
NTIS | 1965
Supersonic Transport Program Phase Iib
NTIS | 1965
Supersonic Transport Program Phase Iic
NTIS | 1965
Supersonic Transport Program Phase Iic
NTIS | 1965