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Wind tunnel tests of a 0.04 scale model of Avro C-105 vertical tail at supersonic speeds

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council of Canada
FormatText, Memorandum
Physical description32 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
Tests have been made in the N.A.E. 30" x 16" high speed wind tunnel on a 0.04 scale model of the vertical tail of the C-105 aircraft to determine the vertical tail load characteristics and rudder hinge moment data. The tests were made at Mach numbers 1.22, 1.35, 1.57, 1.78 and 2.03. The corresponding Reynolds number range is shown in figure 4.
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-46N (October 1957).
Is identical to
  • Conlin, L. T. ‘Wind Tunnel Tests of a 0.04 Scale Model of Avro C-105 Vertical Tail at Supersonic Speeds’. National Research Council of Canada. National Aeronautical Establishment. Aerodynamics, 1957. .
LanguageEnglish
Peer reviewedNo
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Record identifier5a138e71-298f-45ec-8be5-fc7c7ebe7d14
Record created2020-11-26
Record modified2025-03-11
Date modified: