Some Low Speed Problems of High Speed Aircraft-Reference-Cited by-同舟云学术

Some Low Speed Problems of High Speed Aircraft

Published:1962-04 Issue:616 Volume:66 Page:211-225
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Spence A.,Lean D.

Abstract

The high speed aircraft whose low speed aerodynamic problems are discussed in this part of the paper belong to the future rather than to the past or present. Küchemann has shown how jet propulsion and the use of a new set of aerodynamics appropriate to supersonic speed lead one from the classical aircraft to new shapes suitable for achieving a required flight range. These shapes include wing-body arrangements with wing sweepback angles of 55° or 60° suitable for a Mach number of about 1·2, and slender, neartriangular wings with sharp leading edges suitable for Mach numbers of around 2 or more, depending on the ratio of span to length.

Publisher

Cambridge University Press (CUP)

Reference23 articles.

1. Brebner G. G. and Wyatt L. A. (1960). Boundary Layer Measurements at Low Speed on Two Wings of 45° and 55° Sweep. Unpublished M.O.S. paper 1960.

2. Hundleby M. A. An Investigation into the Low Speed Aerodynamic Characteristics of a Family of Slender Wings. Parts I and HI. Rolling Derivatives. A. V. Roe Wind Tunnel Report. Unpublished.

3. Howard M. B. Measurement of Longitudinal and Lateral Stability and Control Powers of a Slender Wing Model at Subsonic Speeds. A. V. Roe Wind Tunnel Report. Unpublished.

4. Garner H. C. and Walshe D. E. (1959). Pressure distribution and Surface Flow on 5% and 9% Thick Wings with Curved Tip and 60° Sweepback. A.R.C. 20982. 1959.

5. Prescott T. W. and Eaton R. Automatic Throttle Control in Avro 707A Aircraft. R.A.E. Technical Note (B.L.E.U.). To be published.

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