H. Starken

发表

H. Starken, 1983 .

An Improved Off-Design Loss Prediction Method for Supercritical Compressor Blades

H. Starken, V. Jawtusch, 1993 .

Discussion: “Transonic Cascade Flow Solved by Separate Supersonic and Subsonic Computations With Shock Fitting” (Wu, Wenquan, Wu, Chung-Hua, and Yu, Dabang, 1985, ASME J. Eng. Gas Turbines Power, 107, pp. 329–335)

H. Starken, 1985 .

Experimental investigation of a supercritical compressor rotor blade section

H. Starken, R. Fuchs, R. Kaymaz, 1987 .

Supersonic cascade flow

H. Starken, H.-J. Lichtfuss, H. Starken, 1974 .

Design, construction and testing of an AGARD standard model D for oscillatory derivatives measurements

H. Starken, 1964 .

Design and Testing of Two Supercritical Compressor Cascades

H. Starken, H. Rechter, P. Schimming, 1979 .

TRANSONIC COMPRESSOR ROTOR CASCADE WITH BOUNDARY-LAYER SEPARATION: EXPERIMENTAL AND THEORETICAL RESULTS

H. Starken, W. Steinert, R. Fuchs, 1993 .

Experimental cascade analysis of a transonic compressor rotor blade section

H. Starken, H. A. Schreiber, H. Starken, 1983 .

Boundary-Layer Separation and Transition Visualized by Liquid Crystal Costing

H. Starken, W. Steinert, 1993 .

Redesign and performance analysis of a transonic axial compressor stator and equivalent plane cascades with subsonic controlled diffusion blades

H. Starken, H. Weyer, H. Rechter, 1984 .

Design and analysis of a high pitch to chord ratio cascade representative of ducted propfans

H. Starken, W. Steinert, A. Weber, 1991 .

Experimental cascade analysis of a transonic compressor rotor blade section

H. Starken, H. A. Schreiber, 1984 .

Redesign and Performance Analysis of a Transonic Axial Compressor Stator and Equivalent Plane Cascades With Subsonic Controlled Diffusion Blades

H. Starken, H. Weyer, H. Rechter, 1983 .

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

H. Starken, W. Steinert, B. Eisenberg, 1990 .

Discussion: “Supersonic Compressor Cascades—An Analysis of the Entrance Region Flow Field Containing Detached Shock Waves” (York, R. E., and Woodard, H. S., 1976, ASME J. Eng. Power, 98, pp. 247–254)

H. Starken, H. J. Lichtfuss, 1976 .

Inlet Flow Angle Determination of Transonic Compressor Cascades

H. Starken, W. Steinert, R. Fuchs, 1991 .

Design and testing of a controlled diffusion airfoil cascade for industrial axial flow compressor application, ASME paper 90-GT-140

H. Starken, W. Steinert, B. Eisenberg, 1991 .

Utilization of Linear Cascade Experiments in Turbomachine Design Development

H. Starken, 1991 .

Design and Analysis of a Highly Loaded Compressor Cascade

H. Starken, W. Steinert, A. Weber, 1993 .

Experimental Investigations of Supersonic Cascades Designed for High Static Pressure Ratios

H. Starken, R. Fuchs, 1977 .

Inlet flow angle determination of transonic compressor cascades

H. Starken, R. Fuchs, W. Steinert, 1992 .

Closure to “Discussions of ‘Some Experimental Results of Two-Dimensional Compressor Cascades at Supersonic Inlet Velocities’” (1971, ASME J. Eng. Power, 93, p. 292)

H. Starken, H. J. Lichtfuss, 1971 .

Performance of Controlled Diffusion Blades

H. Starken, 1992 .

Supersonic Exit Flow of Two-Dimensional Cascades

H. Starken, H. J. Lichtfuss, 1972 .

Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions

H. Starken, V. Jawtusch, A. Weber, 1987 .

Off-Design Transition and Separation Behavior of a CDA Cascade

H. Starken, W. Steinert, 1996 .

Some Experimental Results of Two-Dimensional Compressor Cascades at Supersonic Inlet Velocities

H. Starken, H. J. Lichtfuss, 1970 .

Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application

H. Starken, W. Steinert, B. Eisenberg, 1991 .

Experimental Investigation of the Performance of a Supersonic Compressor Cascade

H. Starken, D. L. Tweedt, H. A. Schreiber, 1988 .