A method of computing the potential flow on thick wing tips

[1]  R. Kress.  Treatment of the Prager Problem of Potential Theory by the Integral Equation Method , 1969 .

[2]  J. Summa.  Potential flow about three-dimensional lifting configurations, with application to wings and rotors , 1975 .

[3]  J. Hess.  Review of integral-equation techniques for solving potential-flow problems with emphasis on the surface-source method , 1975 .

[4]  Theodore Theodorsen,et al.  Theory of wing sections of arbitrary shape , 1933 .

[5]  Michael L. Lopez,et al.  A Theoretical Method for Calculating the Aerodynamic Characteristics of Arbitrary Jet-Flapped Wings. Volume I. The Elementary Vortex Distribution Jet-Wing Lifting Surface Theory. , 1973 .

[6]  H. A. Luther,et al.  Applied numerical methods , 1969 .

[7]  P C Pien.  CALCULATION OF NON-LIFTING POTENTIAL FLOW ABOUT ARBITRARY THREE-DIMENSIONAL BODIES BASED ON DOUBLET DISTRIBUTIONS , 1975 .

[8]  I Lotz,et al.  Calculation of potential flow past airship bodies in yaw , 1932 .

[9]  Ira H. Abbott,et al.  Summary of Airfoil Data , 1945 .

[10]  D. M. Friedman.  Improved solution for potential flow about arbitrary axisymmetric bodies by the use of a higher-order surface source method. Part 2. User's manual for computer program , 1974 .

[11]  J. Hess,et al.  Higher order numerical solution of the integral equation for the two-dimensional neumann problem , 1973 .

[12]  Domina Eberle Spencer,et al.  Field Theory for Engineers , 1964 .

[13]  E. A. Boyd.  Principles of Ideal-Fluid Aerodynamics. K. Karamcheti. John Wiley & Sons Inc.1966. 636 pp. Illustrations. 160s. , 1967 .

[14]  J. Hess,et al.  Calculation of potential flow about arbitrary bodies , 1967 .

[15]  Eastman N. Jacobs,et al.  The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel , 1932 .

[16]  T. Kármán.  Calculation of Pressure Distribution on Airship Hulls , 1930 .

[17]  J. Hess,et al.  The problem of three-dimensional lifting potential flow and its solution by means of surface singularity distribution☆ , 1974 .

[18]  F. Vandrey,et al.  A Method for Calculating the Pressure Distribution of a Body of Revolution Moving in a Circular Path through a Perfect Incompressible Fluid , 1960 .

[19]  J. Hess,et al.  The use of higher-order surface singularity distributions to obtain improved potential flow solutions for two-dimensional lifting airfoils☆ , 1975 .