Account of aerodynamic considerations involved in evolution of new executive or feederliner aircraft and basic design requirements; design specification selected for aircraft seating 6 to 10 executive passengers in comfort or 18 passengers, having range of 1500 mi stage with 5 executive passengers and luggage plus crew of 2, and cruising in 300 mph bracket; field length required is about 1000 yd; description of aircraft, choice of powerplant and propeller; aerodynamic design; schematics and various layouts.
Aerodynamic design philosophy of handley page jetstream
Aircraft Eng
Aircraft Engineering ; 39 , n 9
1967
12 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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