F-111C Longitudinal and Lateral Aerodynamic Flight Data Analysis for Take-off and Landing Configurations.

Abstract

A series of flight trials was performed on an F-111C aircraft, tail number A8-132, at the RAAF's Aircraft Research and Development Unit. Data obtained from the tests has been analysed in Air Operations Division to determine the aircraft aerodynamic and control derivatives. In this report the longitudinal and lateral derivatives for the take-off and landing configurations are presented and compared with wind tunnel results.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1996
Accession Number
ADA311534

Entities

People

  • A. D. Snowden
  • J. S. Drobik

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Air Force
  • Aircrafts
  • Computer Programs
  • Control Systems
  • Data Analysis
  • Data Processing
  • Engineering
  • Equations Of Motion
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Research Facilities
  • Simulators
  • Tactical Aircraft
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Aviation Science / Aeronautics.