Author

Chong‐Wei Chu

Observed names: C. W. CHU, C. W. Chu, C.-W. CHU, CHONG-WEI CHU, Chong-Wei Chu, Chu, Chong-Wei

Observed institution: University of Minnesota

OpenAlex ID: A5009678607

Simple Two-Dimensional-Nozzle Plume Model for Infrared Analysis

1981 · Chong-Wei Chu, Joe Der, et al. · Journal of Aircraft · 18

Compatibility relations and a generalized finite-difference approximation for three- dimensional steady supersonic flow.

1967 · CHONG-WEI CHU · AIAA Journal · 12

Evolution of swirl in two-dimensional-nozzle flow

1982 · Joe Der, Chong-Wei Chu, et al. · Journal of Aircraft · 10

Effect of swirl on the potential core in two-dimensional ejector nozzles

1983 · Chong-Wei Chu, Joe Der, et al. · Journal of Aircraft · 9

Modeling of 2D-nozzle plume for IR signature prediction under static conditions

1981 · C.-W. CHU, J. DER, JR. · AIAA Thermophysics Conference · 6

A simple 2D-nozzle plume model for IR analysis

1980 · C.-W. CHU, J. DER, JR., et al. · Aircraft Systems and Technology Meeting · 6

A simple derivation of three-dimensional characteristic relations

1964 · CHONG-WEI CHU · AIAA Journal · 6

On the impingement of a supersonic jet on a flat plate

1969 · Chong-Wei Chu, S. A. Powers, et al. · Zeitschrift für angewandte Mathematik und Physik · 5

A new algorithm for three-dimensional method of characteristics.

1972 · CHONG-WEI CHU · AIAA Journal · 4

Interaction of two cylindrical jets.

1967 · C. W. CHU, A. F. NIEMANN, et al. · AIAA Journal · 4

Unsteady two-dimensional subsonic transonic, and supersonic flow calculations by the method of characteristics

1976 · Chong-Wei Chu, Stefan Nadir · Lecture notes in physics · 2

Wave Drag Reduction for Aircraft Fuselages.

1975 · Chong‐Wei Chu, Joe Der, et al. · Defense Technical Information Center (DTIC) · 2

Supersonic Flow about Slab Delta Wings and Wing-Body Configurations

1973 · CHONG-WEI CHU · Journal of Spacecraft and Rockets · 2

Equivalence of nonequilibrium flows behind normal and oblique shock waves

1964 · CHONG-WEI CHU · AIAA Journal · 2

A simple analytical method for predicting axisymmetric turbulent jetflowfields in a freestream

1985 · C.-W. CHU · 23rd Aerospace Sciences Meeting · 1

ADEN plume flow properties for infrared analysis

1982 · Chong-Wei Chu, Joe Der · Journal of Aircraft · 1

Expedient approach to nonaxisymmetric nozzle performance prediction

1980 · Chong-Wei Chu · Journal of Aircraft · 1

Calculation of Unsteady Two-Dimensional Supersonic Flow by the Method of Characteristics.

1975 · Chong‐Wei Chu, H. KAO, et al. · Defense Technical Information Center (DTIC) · 1

The Calculation of Three-Dimensional Supersonic Flows around Spherically-Capped Smooth Bodies and Wings. Volume 1. Theory and Application

1972 · Chu, Chong-Wei, Powers, Sidney A. · Defense Technical Information Center (DTIC) · 1

Use of equilibrium constants in nonequilibrium flow computations

1965 · CHONG-WEI CHU · AIAA Journal · 1

On the motion of a magnetically confined plasma cylinder

1964 · Chong-Wei Chu · Quarterly of Applied Mathematics · 1

PDF

A new ejector concept for V/STOL aircraft

1983 · C.-W. CHU, V. ORTIZ, et al.

Wave Drag Reduction for Aircraft Fuselage-Wing Configurations. Volume I. Analyses and Results

1976 · Chong‐Wei Chu, Joe Der, et al. · Defense Technical Information Center (DTIC)

Wave Drag Reduction for Aircraft Fuselage-Wing Configurations. Volume 2. Manual for Computer Programs

1976 · Chong‐Wei Chu, Joe Der, et al.

An inverse problem of nonequilibrium duct flow.

1966 · CHONG-WEI CHU · AIAA Journal

Works count: 29

Citation count: 95

H-index: 6

I10-index: 3