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Wind tunnel investigation of possible rudder flutter on a 1:25 scale fin model of CF-105 at Mach Number of 1.22

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council of Canada
FormatText, Memorandum
Physical description17 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
As the theoretical calculations indicated a possibility of the development of rudder flutter on CF-105, an experimental verification of the critical speed and frequency was required. A series of tests in the NAE 30 in. x 16 in. supersonic wind tunnel was performed on a fin model equipped with rudders of suitable density and hinge stiffness.
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-46k (28 March 1957).
Is identical to
  • Orlik-Ruckemann, K. ‘Wind Tunnel Investigation of Possible Rudder Flutter on a 1:25 Scale Fin Model of CF-105 at Mach Number of 1.22’. National Research Council of Canada. National Aeronautical Establishment. High Speed Aerodynamics, 1957. .
LanguageEnglish
Peer reviewedNo
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Record identifierbb949da3-b717-4e8c-b46e-10163d2f1e14
Record created2020-11-26
Record modified2025-03-07
Date modified: