D. A. Nealy

发表

Development of a Design Model for Airfoil Leading Edge Film Cooling

A. R. Wadia, D. A. Nealy, A. Wadia, 1985 .

Measurements of Heat Transfer Distribution Over the Surfaces of Highly Loaded Turbine Nozzle Guide Vanes

L. D. Hylton, H. J. Gladden, D. A. Nealy, 1984 .

Experimental Simulation of Turbine Airfoil Leading Edge Film Cooling

A. R. Wadia, D. A. Nealy, 1988 .

Periodic report, design of a strut supported turbine vane with a wire-form porous shell

R. D. Anderson, D. A. Nealy, D. Nealy, 1968 .

Erratum: “Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate” (Journal of Engineering for Power, 1973, 95, pp. 319–325)

D. A. Nealy, 1974 .

An Analytical Study of the Effects of Turbine Variable Geometry Operation on Turbine Blade Cooling Requirements for Fixed Match Point Turbojet Application

H. G. Lueders, D. A. Nealy, 1976 .

Closure to “Discussion of ‘Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate’” (1974, ASME J. Eng. Power, 96, pp. 320–321)

D. A. Nealy, 1974 .

Discussion: “The Additive Nature of Film Cooling From Rows of Holes” (Muska, J. F., Fish, R. W., Suo, M., 1976, ASME J. Eng. Power, 98, pp. 457–463)

D. A. Nealy, 1976 .

Evaluation of Laminated Porous Wall Materials for Combustor Liner Cooling

D. A. Nealy, S. B. Reider, D. Nealy, 1979 .

A Note on Turbine Cooling Performance Characterization

D. A. Nealy, 1995 .

Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate

D. A. Nealy, 1973 .