Accession Number : AD0783621
Title : An Approximate Solution of Unsteady Transonic Flow Problems.
Descriptive Note : Technical rept. Jun 73-Jan 74,
Corporate Author : TENNESSEE UNIV SPACE INST TULLAHOMA
Personal Author(s) : Wu,J. M. ; Kimble,K. R.
Report Date : JUN 1974
Pagination or Media Count : 39
Abstract : Unsteady pressures on a thin two-dimensional airfoil pitching and plunging in transonic flow have been computed by numerically solving the governing partial differential equation. The effect of wing thickness has been retained by using the steady flow potential on the wing in the coefficients of the equation in a manner which generalizes Oswatitsch's parabolic method. The results are compared with other methods and with experimental data. (Author)
Descriptors : *Airfoils, *Transonic flow, Control surfaces, Flow fields, Differential equations, Numerical analysis
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE