Aerodynamic Computer Code for Computing Pressure Loading on Wings for Structural Analysis.

Abstract

The report describes the development of an aerodynamic computer code for calculating the pressure distribution on wings and to interpolate by surface fit at locations as specified for structural analysis using the NASTRAN computer code.

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1975
Accession Number
ADA013314

Entities

People

  • Kenneth K. Wang
  • Richard S. Lee

Tags

DTIC Thesaurus Topics

  • Civil Engineering
  • Computers
  • Pressure Distribution
  • Structural Analysis

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Computer Science.
  • Structural Health Monitoring of Composite Structures.