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Six-component supersonic wind tunnel tests of a 1/80 scale model of the C-105 aircraft

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council of Canada
FormatText, Memorandum
Physical description310 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
Six-component supersonic wind tunnel tests were carried out on a 1/80 scale model of the C-105 aircraft at four Mach numbers. In all, 27 model configurations were investigated over a period of three months requiring a total of 1991 tunnel runs. This memorandum contains the results of these tests in the form of basic plots, cross plots and final aerodynamic derivatives. In order to expedite the publication of the data, the results are presented without detailed analysis.
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-46h (31 October 1956).
Is identical to
  • Laberge, J. G. ‘Six-Component Super-Sonic Wind Tunnel Tests of a 1/80 Scale Model of the C-105 Aircraft’. National Research Council of Canada. National Aeronautical Establishment. Aerodynamics, 1956. .
LanguageEnglish
Peer reviewedNo
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Record identifier5e9f9bee-da12-4754-88a2-722a13f9deb3
Record created2020-11-26
Record modified2025-03-11
Date modified: