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Showing 7 out of a total of 17 results for community: Aeronautical Research Council. (0.072 seconds)

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Note on the time required for the achievement of steady flow past a slender body in a hypersonic shock tunnel

D. W. Holder; D. L. Schultz (1961)
Observations of the supersonic flow round a 6 per cent double wedge

D. W. Holder; A. Chinneck; D. G. Hurley (1951)
Observations of the flow round a two-dimensional aerofoil oscillating in a high-speed air stream

A. Chinneck; D. W. Holder; C. J. Berry (1952)
Examples of the effects of shock-induced boundary-layer separation in transonic flight

H. H. Pearcey; D. W. Holder (1954)
Experiments with slotted and perforated walls in a two-dimensional high-speed tunnel

D. W. Holder; R. J. North; A. Chinneck (1951)
On the flow in a reflected-shock tunnel

D. W. Holder; D. L. Schultz (1960)
The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory

D. W. Holder; R. J. North (1949)

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Author
- D. W. Holder (17)
- R. J. North (6)
- A. Chinneck (5)
- D. L. Schultz (2)
- G. E. Gadd (2)
- C. J. Berry (1)
- D. G. Hurley (1)
- H. H. Pearcey (1)
- J. D. Regan (1)
- R. F. Cash (1)
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