Additions and Corrections to 'SUPER': A Program for Calculating Steady and Oscillatory Supersonic Flow Over a Thin Wing, Tail Plane and Fin

Abstract

This paper describes changes to the computer program SUPER, which correct errors identified in the previous version of the program, and enable the calculation of generalised forces. Tables of generalised forces, calculated using SUPER and other programs, are presented for a standard AGARD configuration.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1989
Accession Number
ADA211771

Entities

People

  • I. H. Grundy

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Computer Programs
  • Computers
  • Department Of Defense
  • Flow
  • Horizontal Stabilizers
  • Intellectual Property
  • Leading Edges
  • Lifting Surfaces
  • Mach Number
  • Mathematics
  • Numbers
  • Procedures (Computers)
  • Standards
  • Supersonic Flow
  • Thin Wings

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Computer Science.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics