Accession Number : ADA118388

Title :   Computer Program for Calculation of Airfoil Pressure and Turbulent Friction Drag.

Descriptive Note : Final rept.,

Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIRCRAFT AND CREW SYSTEMS TECHNOLOGY DIRECTORATE

Personal Author(s) : Franz,Joseph J

PDF Url : ADA118388

Report Date : 01 Jul 1977

Pagination or Media Count : 29

Abstract : A computer program has been developed which calculates approximate pressure drag coefficient values of thin symmetrical airfoil sections based on convex airfoil data. Flat plate turbulent friction results are also included for fully developed turbulent flow. (Author)

Descriptors :   *Airfoils, *Computer program documentation, *Aerodynamic drag, *Friction, *Turbulence, Turbulent flow, Computations, Fortran, Subroutines, Transonic flow, Machine coding, Thinness, Symmetry, Input output models

Subject Categories : Aircraft
      Computer Programming and Software
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE