AERADE Home
→
Browsing by Author

Browsing by Author "G. G. Brebner"

Now showing items 1-8 of 8

Boundary layer measurements at low speed on two wings of 45 degrees and 55 degrees sweep

G. G. Brebner; L. A. Wyatt (1961)
The Calculation of the Loading and Pressure Distribution on Cranked Wings

G. G. Brebner (1953)

Using distributions of vortices and sources over the aerofoil surface, approximate formulae are developed for finding the spanwise and chordwise loadings of cranked wings (i.e., wings with discontinuous changes of sweep), ...
The calculation of the spanwise loading of sweptback wings with flaps or all-moving tips at subsonic speeds

G. G. Brebner; D. A. Lemaire (1955)

The results of some electric tank tests by Duquenne and Grandjean on wings of 45 deg sweepback with trailing edge flaps have been analysed to provide the basis for a method of calculating the spanwise loading. The analysis ...
Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section

G. G. Brebner; L. A. Wyatt; Gladys P. Ilott (1967)
Low-Speed Tests on 45-deg Swept-back Wings Parts I and II

J. Weber; G. G. Brebner; D. Kuchemann (1951)

PART I - Pressure Measurements on Wings of Aspect Ratio 5. This report contains the results of pressure measurements on three 45-deg swept-back wings with constant chord and aspect ratio 5, over an incidence range up to ...
Pressure and boundary-layer measurements on a two-dimensional wing at low speed

G. G. Brebner; J. A. Bagley (1952)

Results are given of pressure measurements and boundary-layer traverses on a two-dimensional wing with 10 per cent RAE 101 section at Reynolds numbers of 1.6 x 10power6 and 3.2 x 10power6. These results, which have been ...
Some simple conical camber shapes to produce low lift-dependent drag on a slender delta wing

G. G. Brebner (1959)
The velocities induced by distributions of infinite kinked source and vortex lines representing wings with sweep and dihedral in incompressible flow

G. G. Brebner; L. A. Wyatt (1970)

Equations have been derived for the velocities induced in an incompressible flow by distributions of infinite source and vortex lines representing wings of infinite span and constant chord having both sweep and dihedral. ...

Browsing by Author "G. G. Brebner"

Browsing by Author "G. G. Brebner"

Search AERADE

Browse

All of AERADE

My Account