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Houghton, D.S. (author), Chan, A.S.L. (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 1957
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Houghton, D.S. (author), Chan, A.S.L. (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 1958
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Chan, A.S.L. (author)The fundamental problem of structural design is the deternaination of structures of minimum weight which safely equilibrate a given system of external forces. The classical theorem of Michell gave the basic requirements for such a structure. The first part of this paper analyses the geometrical layout of two-dimensional structures which satisfy...report 1960
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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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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 1964
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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 1964
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- Chan, Y.Y. (author) report 1965
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- Chan, Y.Y. (author), Mason, R.P. (author), Reddy, N.M. (author) report 1965
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- Chan, B.C. (author), Holt, M. (author), Welsh, R.L. (author) report 1966
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Chan, Y.Y. (author)An approximate method of solution for the compressib le laminar boundary layer over a three-dimensional body has been developed. An intrinsic s treamline co-ordinate s ystem is used. The approach is perturbation in nature with the assumption of small cross- flow. Integral methods are then used to solve the resulting equations. In the present...report 1966
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- Chan, Y.Y. (author) report 1967
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Chan, Y.Y. (author)Three-dimensional luminar incompressiblc boundary layers with suction and normal injection are examined. Similarity flows arc considered and similar solutions are obtained numerically. Resul ts show that the cross-flows and, hence, the three-dimensional behaviour of the boundary layer are greatly reduced when sudion is applied, and inversely,...report 1967
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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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- Chan, B.C. (author), Holt, M. (author), Welsh, R.L. (author) journal article 1968
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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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- Chan, Robert K. -C. (author), Strelkoff, Theodor (author) report 1969
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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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Chan, Y.Y. (author)The performance of an augmentor wing has been examined with a simplified model that consists of a thin airfoil with a jet-augmented flap and a sink located at the hinge of the flap. The analysis is based on a small disturbance theory. The results for the basic configuration, namely the airfoil with a jet-augmented flap, agree very well with...report 1969
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Chan, Y.Y. (author)A computational method for turbulent boundary layers in an incompressible two-dimensional flow has been formulated. The governing differential equations for the mean flow are solved by an implicit finite difference method. The Reynolds shear stress is correlated by Prandtl's mixing length concept. Four models of correlation for the mixing length...report 1970
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- Chan, S.K. (author), Cappelli, G. (author), Graf, W.O. (author) report 1971