On the Flow Past a Circular Jet Exhausting at Right Angles from a Flat Plate or Wing-Reference-Cited by-同舟云学术

On the Flow Past a Circular Jet Exhausting at Right Angles from a Flat Plate or Wing

Published:1967-03 Issue:675 Volume:71 Page:216-218
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Wooler P. T.

Abstract

In recent years there has been considerable interest in the possibility of providing high speed aircraft with the capability of vertical or short take-off and landing (V/STOL). One method for achieving V/STOL is to use lifting engines or fans, the aerodynamic interference effects of which are not yet fully understood. Experimental work on this problem has been done by Jordinson, Otis, Vogler and research workers at the British Aircraft Cor-poration, but no satisfactory theoretical analysis is known. The object of this paper is to put forward a semi-empirical method for predicting the aerodynamic interference of an exhausting jet on a uniform mainstream flow past a wing.

Publisher

Cambridge University Press (CUP)

Reference9 articles.

1. Wyatt L. A. Some Tests of Ground Effect on Plan-forms Fitted with a Centrally Located Round Lifting Jet. RAE Report No Aero 2826, June 1962.

2. Unpublished Wind Tunnel Results. British Aircraft Corporation (Operating) Limited, Preston Division.

3. Vogler R. D. Surface Pressure Distributions Induced on a Flat Plate by a Cold Air Jet Rising Perpendicularly from the Plate and Normal to a Low-Speed Free-Stream Flow. NASA TN D-1629, March 1963.

4. Base T. E. Lift and Pitching Momentum Increments due to Engines Mounted at an Angle to the Free Stream in a Nacelle or Wing. Bristol Aircraft Aero Note 95, June 1962.

5. Falkner V. M. The Calculation of the Aerodynamic Loading on a Surface of any Shape. ARC R and M 1910, 1943.

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