analysis indicating the effect of increasing the block speed on the aircraft's productivity and economy on a particular route network.
The industrial activities aimed at development of new SCT applications were concentrated in the time frame 1960–1990 but, in spite of the long history of technological research and development on civil supersonic aircraft, little systematic information required to initiate a realistic conceptual design of a supersonic transport or executive jet has been published. Remarkable exceptions are Corning's textbook [2] appearing first in 1960 with later versions up to 1976, and [3] published in 1978. Küchemann's authoritative book is dedicated to the aerodynamic design of transport aircraft in general and Concorde's aerodynamic development in particular.
The Concorde would not be able to successfully comply with the requirements of commercial air transport in the 21st century but with the present‐day technologies a much more efficient supersonic transport than the Concorde could be built. Many projects have been started to investigate the viability of a second generation SCT, resulting in a wealth of articles written by investigators from all continents, together forming a deluge for (teams of) engineers who are supposed to create a design concept based on a realistic set of top level requirements. It is the intention of the present author to present a synthesis of classical analysis models as well as methodologies generated by recent technological research and project studies that can be considered as an essential guidance to conceive an initial configuration design.
Bibliography
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Note
1 1 The transonic area rule describes how the variation of the cross‐sectional area along the longitudinal axis can be manipulated to reduce the wave drag of a flight vehicle at near‐sonic and supersonic flight speeds. The results of this design methodology are often manifest in highly swept wings and “coke bottle” shaped fuselages.
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