The USAF Stability and Control Digital DATCOM. Volume I. Users Manual

Abstract

This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in the USAF Stability and Control Datcom (revised April 1976). Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume I is the user's manual and presents program capabilities, input and output characteristics, and example problems. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1979
Accession Number
ADA086557

Entities

People

  • John E. Williams
  • Steven R. Vukelich

Organizations

  • McDonnell Douglas

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Air Force
  • Aircrafts
  • Airfoils
  • Boundary Layer
  • Control Systems Engineering
  • Flaps (Control Surfaces)
  • Geometry
  • High Lift
  • High Lift Devices
  • Horizontal Stabilizers
  • Jet Flaps
  • Operating Systems
  • Split Flaps
  • Stabilization Systems
  • Swept Wings

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.