Accession Number:

ADA055263

Title:

An Automated Procedure for Computing the Three-Dimensional Transonic Flow Over Wing-Body Combinations, Including Viscous Effects. Volume III. An Implicit Method for the Calculation of Three-Dimensional Boundary Layers on Finite, Thick Wings.

Descriptive Note:

Final rept. 1 May 75-1 Oct 77,

Corporate Author:

GRUMMAN AEROSPACE CORP BETHPAGE N Y

Personal Author(s):

Report Date:

1977-02-01

Pagination or Media Count:

95.0

Abstract:

This volume contains the theory and description of the code of a new three-dimensional boundary layer program that computes the laminar and turbulent boundary layers over finite thick wings. Author

Subject Categories:

  • Aircraft
  • Computer Programming and Software
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE