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Showing 10 out of a total of 17 results for community: Aeronautical Research Council. (0.132 seconds)

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Observations of the interaction between the shock waves and boundary layers at the trailing edges of aerofoils in supersonic flow

D. W. Holder; R. J. North (1951)
The high-speed laboratory of the aerodynamics Division, N.P.L. Part I - description of the installation. Part II - experimental techniques. Part III - experimental results.

D. W. Holder (1946)
Experiments with static tubes in a supersonic airstream -- parts 1 and 2

D. W. Holder; R. J. North; A. Chinneck (1950)
Experiments with a two-dimensional aerofoil designed to be free from turbulent boundary-layer separation at small angles of incidence for all mach numbers

D. W. Holder; R. F. Cash (1957)
Schlieren methods for observing high-speed flows

D. W. Holder; R. J. North (1954)
Note on the flow near the tail of a two-dimensional aerofoil moving at a free-stream mach number close to unity

D. W. Holder (1955)
Pressure measurements in a supersonic tunnel on a two-dimensional aerofoil of R.A.E. 104 section

D. W. Holder; A. Chinneck; R. J. North (1951)
Base pressures in supersonic flow

G. E. Gadd; D. W. Holder; J. D. Regan (1956)
A note on shock tubes

D. W. Holder (1953)
Boundary layer separation in two-dimensional supersonic flow

G. E. Gadd; D. W. Holder (1956)

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- 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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