Low-speed tests on a two-dimensional unswept wing with a 10 per cent thick RAE 101 section

von Crabtree, L. F.
Veröffentlicht in Crabtree, L. F. The formation of regions of separated flow on wing surfaces (1959)

Laminar-separation bubbles and the mechanism of the leading-edge stall

von Crabtree, L. F.
Veröffentlicht in Crabtree, L. F. The formation of regions of separated flow on wing surfaces (1959)

The rotating flap as a high-lift device

von Crabtree, L. F.
Veröffentlicht 1960

The formation of regions of separated flow on wing surfaces

von Crabtree, L. F.
Veröffentlicht 1959

The range performance of hypersonic aircraft

von Peckham, D. H.
Veröffentlicht 1967

The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough

Design, instrumentation and flow visulization techniques

von Crabtree, L. F.
Veröffentlicht in Crane, J. F. W. The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough ; Pt. 1, 2, & 3 (1962)

The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough

von Crane, J. F. W.
Veröffentlicht 1962

Estimation of heat transfer to flat plates, cones and blunt bodies

von Crabtree, L. F.
Veröffentlicht 1970

A semi-empirical prediction method for pressures on the windward surface of circular cones at incidence at high supersonic and hypersonic speeds (M=3)

von Collingbourne, J. R.
Veröffentlicht 1965