Language selection

Government of Canada / Gouvernement du Canada

Search

A summary of high speed wind tunnel test results for the Avro CF-105, and their effects on estimated performance

From National Research Council Canada

AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council Canada
FormatText, Memorandum
Physical description31 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
This note compares some of the results of model tests on the CF-105, which were carried out in the Cornell transonic tunnel, in the 4 ft. wind tunnels at NACA, Langley, and in the 16 inch x 30 inch high speed tunnel at the NAE. These results are also compared with estimates which were previously made by Avro and NAE of various items which affect performance.
Publication date
PublisherNational Research Council Canada. National Aeronautical Establishment. Aerodynamics
Series
  • Laboratory Memorandum (National Research Council Canada. National Aeronautical Establishment. Aerodynamics), no. AE-46i (11 January 1957).
Is identical to
  • Templeton, R. J., and O. E. Michaelsen. ‘A Summary of High Speed Wind Tunnel Test Results for the Avro CF-105, and Their Effects on Estimated Performance’. National Research Council Canada. National Aeronautical Establishment. Aerodynamics, 1957. .
LanguageEnglish
Peer reviewedNo
Export citationExport as RIS
Report a correctionReport a correction (opens in a new tab)
Record identifier4929c498-013a-4606-a8bf-03ecdab1abfd
Record created2020-11-26
Record modified2025-12-04
Date modified: