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Investigation of effects of ramp span and deflection angle on laminar boundary-layer separation at mach 10.03

L. E. Putnam

NASA Technical Reports Server (NASA) · 1965 · 10 citations · 6 references

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Abstract

Ramp span and deflection angle effects on laminar boundary layer separation at hypersonic speed

References

6

The Interaction of an Oblique Shock Wave with a Laminar Boundary Layer

Raimo J. Hakkinen, Isaac Greber, Leon Trilling et al. · NASA Technical Reports Server (NASA) · 1959 · 191 citations · Full text

, , +16

An experimental investigation of the interaction between shock waves and boundary layers

Geoffrey Michael Gadd, Douglas William Holder, J. Regan · Proceedings of the Royal Society of London A Mathematical and Physical Sciences · 1954 · 84 citations

Mach 8 to 22 studies of flow separations due to deflected control surfaces

D. MILLER, R. HIJMAN, M. E. Childs · AIAA Journal · 1964 · 66 citations

, , +7

A Theoretical Investigation of Laminar Separation in Supersonic Flow

Geoffrey Michael Gadd · Journal of the aeronautical sciences. [REQUEST TITLE] · 1957 · 29 citations

, , +4

Some Experiments on Hypersonic Separated Flows

S. M. Bogdonoff, I. E. Vas · ARS journal · 1962 · 29 citations

, , +4