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Estimated lift and drag characteristics of four wings at supersonic speeds

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council of Canada
FormatText, Memorandum
Physical description11 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
Empirical methods of estimating the lift and drag characteristics of untwisted and uncambered wings at supersonic speeds have been developed in the Aerodynamics Laboratory. These methods are applied in the present note to the estimation of the characteristics of four wings at present undergoing force tests in the 10-inch supersonic tunnel.
Publication date
PublisherNational Research Council of Canada. National Aeronautical Establishment. Aerodynamics
Series
  • Laboratory Memorandum (National Research Council of Canada. National Aeronautical Establishment. Aerodynamics), no. AE-45 (4 June 1953).
Is identical to
  • Templin, R. J. ‘Estimated Lift and Drag Characteristics of Four Wings at Supersonic Speeds’. National Research Council of Canada. National Aeronautical Establishment. Aerodynamics, 4 June 1953. .
LanguageEnglish
Peer reviewedNo
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Record identifier831304f2-68ac-4f10-bab2-5d628af4c8eb
Record created2020-11-23
Record modified2025-03-11
Date modified: