D. K. Hennecke

发表

Local and Average Transfer Coefficients due to Different Impingement Arrangements for Blade Cooling Applications

U. Pagenkopf, D. K. Hennecke, 1994 .

Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part II — A Model for Supersonic Flow

D. K. Hennecke, W. M. König, L. Fottner, 1994 .

Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part II—A Model for Supersonic Flow

D. K. Hennecke, L. Fottner, W. M. König, 1996 .

Turbine tip clearance control in gas turbine engines

D. K. Hennecke, K. Trappmann, 1983 .

Transient thermal behaviour of a compressor rotor with ventilation. Test results under simulated engine conditions

D. K. Hennecke, E. Reile, U. Radons, 1985 .

HEAT TRANSFER PROBLEMS IN AERO-ENGINES

D. K. Hennecke, D. Hennecke, 1988 .

Temperature Depression at the Base of a Fin

Ephraim M Sparrow, D. K. Hennecke, D. Hennecke, 1970 .

Local heat sink on a convectively cooled surface—application to temperature measurement error

Ephraim M Sparrow, D. K. Hennecke, D. Hennecke, 1970 .

The Influence of Rotation on Impingement Cooling

D. K. Hennecke, D. Hennecke, Ch. Mattern, 1996 .