A Calculator Program for Analyzing Airloads on a Wing of Arbitrary Planform and Camber in Subsonic Flow.

Abstract

A subsonic airloads program for small (8-K) calculators is presented. Features include good man-machine interaction and quick turn-around which speed preliminary design. The program is written in BASIC for the HP9830 or HP9831 calculator systems equipped with Matrix ROM and 9862A plotter. Programming techniques illustrated may be applied to any small system having special function keys or an equivalent capability. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1978
Accession Number
ADA054180

Entities

People

  • John C. Sparks

Organizations

  • Flight Dynamics Laboratory

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Space

DTIC Thesaurus Topics

  • Aerospace Craft
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airframes
  • Animal Structures
  • Mach Number
  • Mechanics
  • Military Aircraft
  • Pressure Distribution
  • Structural Integrity
  • Structural Mechanics
  • Subsonic Flow
  • Swept Wings
  • Trailing Edges
  • Wind Tunnel Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.