document

Computer studies of finite-amplitude water waves

Chan, Robert K. -C. (author), Strelkoff, Theodor (author)

report 1969

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A note on a simularity transformation for three-dimensional compressible laminar boundary equations

Chan, Y.Y. (author)

A combined compressibility and similarity transformatian has been derived for the equatians of three-dimensional laminar boundary layers in compressible flow. The resulting equations closely resemble the corresponding equations for incompressible flow. Because of the coupling of the temperature field in the momentum equations. it is not possible...

report 1967

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Integral methods in compressible lamnar boundary layers and their application to hypersonic pressure interactions

Chan, Y.Y. (author)

report 1965

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Instrumentation and calibration of UTIAS 11 in x 15 in. hypersonic shock tunnel

Chan, Y.Y. (author), Mason, R.P. (author), Reddy, N.M. (author)

report 1965

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A simple model of shock cell noise generation and its reduction

Chan, Y.Y. (author)

Based on the data of near field surveys of the sound pressure from a choked jet, a simple model is proposed for the mechanism of the screech generation. A convected wave propagates downstream along the jet boundary and is modulated by its interaction with the shock-expansion waves of the jet. These interactions generate strongdipoleradiations....

report 1972

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Small cross-flows in three-dimensional laminar boundary layers with suction or injection

Chan, Y.Y. (author)

Three-dimensional laminar boundary layers with suction or injection are examined by using an approximate method based on a small cross-flow assumption. The basic equations are derived in detail and the computational method is developed. The method is tested against exact solutions and is found to be reasonably accurate. Two examples with the...

report 1969

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Parametric approximation for incompressible laminar boundary layers with suction of injection

Chan, Y.Y. (author)

The parametric method of Loitsianskii in the theory of laminar boundary layers is extended to include suction or injection at the surface. The universal equation is generalized to include the suction parameters. A power series solution of the universal equation in terms of two parameters, namely, the external velocity gradient and the surface...

report 1968

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Turbulent nonbuoyant or buoyant jets discharged into folowing or quiescent fluids

Chan, Tzeng-Long (author), Kennedy, John F. (author)

report 1972

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Koeling en conditionering van kleine laadeenheden

Chan, Y.S. (author)

report 2001

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An analytical and experimental study of an implosion-driven shock tube

Chan, S.K. (author)

report 1973

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De inklapbare container. Verificatie hangstangconcept

Chan, Y.S. (author)

report 2002

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Analysis of experimental data for cast 10-2/DOA2 supercritical airfoil at high Reynolds numbers

Chan, Y.Y. (author)

Experimental data obtained in the NAE Two-Dimensional Test Facility for CAST 10-2jDOA2 supercritical airfoil have been analyzed for the effects of Reynolds number, transition fixing and Mach number. The data were obtained for Reynolds numbers from 6 to 30 million and Mach numbers from 0.3 to 0.8 with fixed and free transitions. The analysis...

report 1988

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Explosions due to pressurized spheres at the ocean surface

Chan, B.C. (author), Holt, M. (author), Welsh, R.L. (author)

report 1966

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Optimum Michell frameworks for three parallel forces

Chan, H.S.Y. (author)

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

report 1963

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An experimental study of the transonic equivalence rule with lift

Chan, Y.Y. (author)

The transonic equivalence rule with lift has been studied experimentally. Under the conditions defined by the rule, wing-body models with the same cross-sectional area distribution but with wings of different aspect ratios and thicknesses were tested at transonic speeds. The correlations of the lift depending wave drag and the lift parameter for...

report 1982

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The effect of pressure gradient and external turbulence on heat transfer to a cold flat plate

Consigny, H. (author), Chan, C.K. (author), Richards, B.E. (author)

This note presents measurements of heat transfer to a cold surface at conditions simulating advanced aircraft gas turbine flow conditions. They were obtained under isothermal wall conditions in a short duration isentropic light piston tunnel using surface temperature transient techniques. The effects of external turbulence and strong favourable...

report 1979

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Nonlinear spatial wave development in an axisymmetrical turbulent jet

Chan, Y.Y. (author)

This report gives the detailed analysis of the nonlinear development of a spatial-growth wave disturbance in the turbulent shear layer of a circular jet. A concise version of the present problem has been published in the Physics of Fluids (Ref. 2). The method of analysis is based on the global consideration of the energy transfer between the...

report 1975

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De inklapbare container. Verificatie hangstangconcept (summary)

Chan, Y.S. (author)

report 2002

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Analysis of experimental data for cast 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow

Chan, Y.Y. (author)

The experimental investigation of CAST 10-2/DOA 2 supercritical airfoil previously conducted in the NAE Two-Dimensional Test Facility has been extended to low Reynolds number range at the design Mach number 0.765. The results indicate that with forward transition fixing, the data trend at low Reynolds number is different from that at high...

report 1989

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A note on a similarity transformation for three dimensional compressible laminar boundary layer equations

Chan, Y.Y. (author)

report 1967