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Minimum drag tests on the C-105 1/80 scale model

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council Canada
FormatText, Memorandum
Physical description7 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
Zero lift drag measurements of a 1/80 scale model of the C-105 aircraft were made in the 30-inch tunnel at subsonic and supersonic speeds. The Mach number range extended from 0.53 to 1.57 corresponding to a Reynolds number range of 1.2 to 1.7 x 10⁶ based on wing mean aerodynamic chord, see Fig. 1.
Publication date
PublisherNational Research Council Canada. National Aeronautical Establishment. Aerodynamics
Series
  • Laboratory Memorandum (National Research Council Canada. National Aeronautical Establishment. Aerodynamics), no. AE-46b (31 May 1955).
Is identical to
  • Laberge, J. G. ‘Minimum Drag Tests on the C-105 1/80 Scale Model’. National Research Council Canada. National Aeronautical Establishment. Aerodynamics, 1955. .
LanguageEnglish
Peer reviewedNo
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Record identifier4ce9db02-546a-4d0d-99d2-758791105ad5
Record created2020-11-26
Record modified2025-12-04
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