A. M. Cary

发表

Engineering prediction of turbulent skin friction and heat transfer in high-speed flow

M. H. Bertram, A. M. Cary, 1974 .

Turbulent-boundary-layer heat-transfer and transition measurements with surface cooling at Mach 6

A. M. Cary, 1970 .

Slot injection for skin-friction drag reduction

D. M. Bushnell, J. N. Hefner, A. M. Cary, 1977 .

Discrete sonic jets used as boundary-layer trips at Mach numbers of 6 and 8.5

D. R. Stone, A. M. Cary, 1972 .

Drag reduction characteristics of small amplitude rigid surface waves

Dennis M. Bushnell, A. M. Cary, L. M. Weinstein, 1980 .

Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5

J. B. Anders, W. D. Harvey, A. M. Cary, 1975 .

Heat transfer to wavy wall in hypersonic flow.

J. P. Arrington, M. H. Bertram, A. M. Cary, 1967 .

An investigation of film-cooling effectiveness and skin friction in hypersonic turbulent flow

J. N. Hefner, A. M. Cary, 1971 .

Mixing length in low Reynolds number compressible turbulent boundary layers

A. M. Cary, D. Bushnell, B. Holley, 1975 .

Calculation methods for compressible turbulent boundary layers

A. M. Cary, D. Bushnell, J. E. Harris, 1976 .

Summary of available information on Reynolds analogy for zero-pressure-gradient, compressible, turbulent-boundary-layer flow

A. M. Cary, 1970 .

Sustained Small Oscillations in Nonlinear Control Systems

A. M. Cary, D. Bushnell, B. Holley, 1975 .

Effect of two-dimensional multiple sine-wave protrusions of the pressure and heat-transfer distributions for a flat plate at Mach 6

A. M. Cary, E. Morrisette, 1968 .

Turbulent boundary-layer heat transfer and transition measurements for cold-wall conditions at Mach 6.

A. M. Cary, 1968 .