Aerodynamic Computer Code for Computing Pressure Loading on Complete Missile for Structural Analysis.

Abstract

Aerodynamic computer code for calculating the pressure distribution on missile or its components e.g., body and wings and to interpolate by surface fit at locations as specified for structural analysis using the NASTRAN computer code. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1978
Accession Number
ADA048840

Entities

People

  • Kenneth K. Wang

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Computer Programs
  • Computers
  • Coordinate Systems
  • Equations
  • Geometry
  • Instruction Set Architecture
  • Leading Edges
  • Mach Number
  • Operating Systems
  • Physics Laboratories
  • Plastic Explosives
  • Pressure Distribution
  • Punched Cards
  • Structural Analysis
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.