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Tests on .04 scale Arrow Pin Model with I.R. Seeker Pod at supersonic speeds

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council of Canada
FormatText, Memorandum
Physical description29 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 NAE 30" x 16" high speed wind tunnel on a .04 scale model of the vertical tail of the Avro Arrow aircraft to determine the effect of the I.R. seeker pod on the vertical tail characteristics and on rudder hinge moments. The tests were made at Mach numbers 1.35, 1.78 and 2.03. The corresponding Reynolds number range was between 2.36 and 1.98 x 10⁶.
Publication date
PublisherNational Research Council of Canada. National Aeronautical Establishment. High Speed Aerodynamics
Series
  • Laboratory Memorandum (National Research Council of Canada. National Aeronautical Establishment. High Speed Aerodynamics), no. AE-46p (11 September 1958).
Is identical to
  • Conlin, L. T. ‘Tests on .04 Scale Fin Model with I.R. Seeker Pod at Supersonic Speeds’. National Research Council of Canada. National Aeronautical Establishment. High Speed Aerodynamics, 1958. .
LanguageEnglish
Peer reviewedNo
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Record identifier3e6115c6-2043-443c-9225-4dd26119ddf1
Record created2020-11-26
Record modified2025-03-07
Date modified: