Use of Wind Tunnel Model Data in Aerodynamic Design-Reference-Cited by-同舟云学术

Use of Wind Tunnel Model Data in Aerodynamic Design

Published:1951-01 Issue:481 Volume:55 Page:1-26
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Hills R.

Abstract

The 805th Lecture to be read before the Royal Aeronautical Society was given on 19th October 1950 at the Institution of Civil Engineers, Great George Street, London. Major G. P. Bulman, C.B.E., F.R.Ae.S., President of the Society, presided during the first part of the meeting and introduced the Lecturer, Mr. R. Hills, B.A., A.F.R.Ae.S., who had been engaged for some years on low and high speed tunnel work and was in charge of the No. 2 eleven and a half foot tunnel at the Royal Aircraft Establishment, Farnborough.

Publisher

Cambridge University Press (CUP)

Reference8 articles.

1. Jacobs and Sherman . Airfoil section characteristics as affected by variations of the Reynolds number. N.A.C.A. Report No. 586, 1937.

2. Loftin and Smith . Aerodynamic characteristics of 15 N.A.C.A. airfoil sections at seven Reynolds numbers from 0.7 x 106 to 9.0 x 106. N.A.C.A. Technical Note No. 1945, Oct. 1949.

3. The use of model data in aeroplane design;Bradfield;Journal of the Royal Aeronautical Society,1939

4. Maclachlan and Letko . Correlation of two experimental methods of determining rolling characteristics of unswept wings. N.A.C.A. Technical Note 1309, 1947

5. Ackeret Feldman and Rott . Investigations on compression shocks and boundary layers in fast moving gases. Institute for Aerodynamics E.T.U., Zurich, No. 10, 1946.

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