Aerodynamic Design: A Description of the Design Philosophy as It Applies to Performance Requirements, Wings, Flaps, Engine Installations, Tail and Flying Controls
B.J. Prior B.Sc.(Eng.), A.C.G.I., D.I.C., A.F.R.Ae.S.
(Assistant Chief Aerodynamicist, Vickers‐Armstrongs (Aircraft) a member of British Aircraft Corporation, Weybridge,)
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Abstract
THE overall design philosophy of the DAC One‐Elcvcn has already been described in the preceding papers on operating economics and systems—so that this article sets out to extend that information by explaining how the aerodynamic features of the aircraft enable the spscification of this short‐range twin jet to be met.
Citation
Prior, B.J. (1963), "Aerodynamic Design: A Description of the Design Philosophy as It Applies to Performance Requirements, Wings, Flaps, Engine Installations, Tail and Flying Controls", Aircraft Engineering and Aerospace Technology, Vol. 35 No. 5, pp. 149-152. https://doi.org/10.1108/eb033733
Publisher
:MCB UP Ltd
Copyright © 1963, MCB UP Limited