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Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7119

Document Type: Report
Title: The effect of the sweepback of delta wings on the performance of an aircraft at supersonic speeds
Authors: Robinson, A.
Davies, F.T.
Issue Date: Mar-1947
Abstract: The variation with sweepback of total drag of an aircraft in level flight at supersonic speeds is calculated. It is shown that sweepback is not uniformly beneficial, but that in general the optimum amount of sweepback depends in the design speed and altitude.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7119
Appears in Collections:College of Aeronautics Reports

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