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.

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)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1977
Accession Number
ADA055263

Entities

People

  • John Nash
  • Roy Scruggs

Organizations

  • Grumman

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Coordinate Systems
  • Euler Equations
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Mechanical Properties
  • Mechanics
  • Pressure Distribution
  • Shear Stresses
  • Stresses
  • Turbulent Flow
  • Two Dimensional
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.