Hostname: page-component-cd9895bd7-q99xh Total loading time: 0 Render date: 2024-12-28T08:10:59.205Z Has data issue: false hasContentIssue false

Use of Wind Tunnel Model Data in Aerodynamic Design

Published online by Cambridge University Press:  28 July 2016

Extract

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.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1951

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Bradfield, and Ellis, . The use of model data in aeroplane design. Journal of the Royal Aeronautical Society, Vol. XLIII, No. 344, Aug. 1939.Google Scholar
2. Nissen, Gadeberg, and Hamilton, . Correlation of the drag characteristics of a typical pursuit airplane obtained from high-speed wind tunnel and flight tests. N.A.C.A. Report No.916, 1948.Google Scholar
3. Jacobs, and Sherman, . Airfoil section characteristics as affected by variations of the Reynolds number. N.A.C.A. Report No. 586, 1937.Google Scholar
4. 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.Google Scholar
5. Thom, and Perring, . The design and work of the Farnborough High-Speed Tunnel. Journal of the Royal Aeronautical Society, Vol. 52, No. 448, April 1948.CrossRefGoogle Scholar
6. 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.Google Scholar
7. Maclachlan, and Letko, . Correlation of two experimental methods of determining rolling characteristics of unswept wings. N.A.C.A. Technical Note 1309, 1947 Google Scholar
8. Seddon, J. Air Intake Design for High Speed Aircraft. Unpublished. 1950 Google Scholar