Effect of axisymmetric endwall contouring on the high-load low-reaction transonic compressor rotor with a substantial meridian contraction

The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines

J. D. Denton · Journal of Turbomachinery · 1993 · 1.6K citations

Engineering, Mechanical Engineering, Physics +17

Design and overall performance of four highly loaded, high speed inlet stages for an advanced high-pressure-ratio core compressor

L. Reid, R. D. Moore · NASA Technical Reports Server (NASA) · 1978 · 323 citations

Engineering, Aerospace Engineering, Design Optimization +14

Nonaxisymmetric Turbine End Wall Design: Part II—Experimental Validation

Jonathan Hartland, D. G. Gregory-Smith, N. W. Harvey et al. · Journal of Turbomachinery · 1999 · 134 citations · Full text

Engineering, Aerospace Engineering, Aerodynamics +13

The exploitation of three-dimensional flow in turbomachinery design

J. D. Denton, Li Xu · Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science · 1998 · 124 citations

Engineering, Aerospace Engineering, Aerodynamics +13

A Numerical Study of Flow and Heat Transfer in a Smooth and Ribbed U-Duct With and Without Rotation

Yanli Lin, T. I‐P. Shih, Mark A. Stephens et al. · Journal of Heat Transfer · 2000 · 112 citations

Engineering, Computational Engineering, Mechanical Engineering +17