Concepedia

Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

R. W. Cubbison, B. W. Sanders

NASA Technical Reports Server (NASA) · 1968 · 21 citations · 1 references

Concepts

Abstract

Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect of axisymmetric compression

References

1

Effect of porous bleed in a high performance axisymmetric, mixed compression inlet at Mach 2.50

R. W. Cubbison, D. Johnson, E. T. Meleason · NASA Technical Reports Server (NASA) · 1968 · 30 citations

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