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Showing 10 out of a total of 10 results for community: Aeronautical Research Council. (0.122 seconds)

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Factors affecting the performance of the nozzle of a hypersonic shock tube

B. D. Henshall; G. E. Gadd (1956)
A review of theoretical work relevant to the problem of heat transfer effects on laminar separation

G. E. Gadd (1957)
The effects of convex surface curvature on boundary layer separation in supersonic flow

G. E. Gadd (1956)
A note on the theory of the stanton tube

G. E. Gadd (1958)
The interaction between a weak normal shock wave and a turbulent boundary layer

G. E. Gadd (1959)
Base pressures in supersonic flow

G. E. Gadd; D. W. Holder; J. D. Regan (1956)
The numerical integration of the laminar compressible boundary layer equations, with special reference to the position of separation when the wall is cooled

G. E. Gadd (1957)
Boundary layer separation in two-dimensional supersonic flow

G. E. Gadd; D. W. Holder (1956)
Heat-transfer and skin-friction measurements at a mach number of 2.44 for a turbulent boundary layer on a flat surface and in regions of separated flow

G. E. Gadd; W. F. Cope; J. L. Attridge (1958)
Flow in the laminar boundary layer near separation

B. S. Stratford; G. E. Gadd (1954)

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- G. E. Gadd (10)
- D. W. Holder (2)
- B. D. Henshall (1)
- B. S. Stratford (1)
- J. D. Regan (1)
- J. L. Attridge (1)
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