摘要: For several decades (1920’s to 1960’s) the development trend of commercial aviation was higher and faster culminating in 707 class conventional takeoff landing (CTOL) transport (and subsequent derivatives). This extraordinary marriage swept wing jet engines revolutionized long-haul passenger supplanted steam ships trains more recently even eroded lower end spectrum buses. The abruptly halted early ‘70s by a combination economic reality environmental concerns. next logical step beyond aircraft would have been supersonic (SST) or as they are termed today high-speed civil (HSCT). Such an cruises Mach number 2 3 range represent revolutionary long distance transport. An version such Concorde while technological marvel for its time has not proven be economically viable only small were produced operated. U.S. SST program canceled era of: (a) general antipathy (b) sharply rising fuel costs (c) sensitivity/concern. Today there is resurgence interest civilian aircraft.
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D. KÜCHEMANN, AIRCRAFT SHAPES AND THEIR AERODYNAMICS FOR FLIGHT AT SUPERSONIC SPEEDS Advances in Aeronautical Sciences#R##N#Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12–16 September 1960. pp. 221- 252 ,(1962) , 10.1016/B978-0-08-006550-2.50019-3
L. Gaudet, K. G. Winter, Measurements of the Drag of Some Characteristic Aircraft Excrescences Immersed in Turbulent Boundary Layers ,(1973)
Arthur G. Powel, Tom A. Kinard, Shreekant Agrawal, Supersonic boundary layer stability analysis with and without suction on aircraft wings ,(1989)
M. R. Malik, COSAL: A black-box compressible stability analysis code for transition prediction in three-dimensional boundary layers NASA STI/Recon Technical Report N. ,vol. 84, pp. 28002- ,(1982)
C. Driver, D. J. Maglieri, The impact of emerging technologies on an advanced supersonic transport ,(1986)
F. T. Mcquilkin, Feasibility of SPF/DB titanium sandwich for LFC wings ,(1982)
Frances E. Sabo, Jerry N. Hefner, Research in Natural Laminar Flow and Laminar-Flow Control, part 1 ,(1987)
Werner Pfenninger, Chandra S. Vemuru, Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings SAE Technical Paper Series. ,(1988) , 10.4271/881397
D. M. Bushnell, M. R. Malik, Application of Stability Theory to Laminar Flow Control-Progress and Requirements Springer, New York, NY. pp. 1- 17 ,(1987) , 10.1007/978-1-4612-4724-1_1
K. R. Czarnecki, The problem of roughness drag at supersonic speeds ,(1966)