UNSTEADY AERODYNAMIC FORCES FOR GENERAL WING/CONTROL-SURFACE CONFIGURATIONS IN SUBSONIC FLOW. PART II. DIGITAL COMPUTER PROGRAMS,

Abstract

A user's manual and program description are presented for a subsonic kernel-function procedure for the prediction of oscillatory pressure distributions on finite-aspect-ratio wings with partial-span control surfaces. The report contains a listing of the complete Fortran IV digital computer program, a description of the functioning of the various program subroutines, input instructions and output description. Application of the program is illustrated by the input and output for a sample problem. Also contained in this report are recommendations for program usage, including descriptions of certain parameters which have been left unspecified to enhance the versatility and long-term usefulness of the program.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1967
Accession Number
AD0831748

Entities

People

  • J. B. Smedfjeld
  • J. H. Berman
  • P. Shyprykevich

Organizations

  • Grumman

Tags

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aspect Ratio
  • Computer Programs
  • Computers
  • Control Surfaces
  • Digital Computers
  • Kernel Functions
  • Pressure Distribution
  • Procedures (Computers)
  • Subsonic Flow
  • Surfaces

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Computer Science.