A-37B Elevator Trim Tab Test and Variable Bobweight Flying Qualities Evaluation.

Abstract

The purpose of this test program was to determine the maximum aircraft nosedown trim tab required for the A-37B aircraft and to compare the handling qualities with the variable bobweight connected and disconnected from the flight control system.

Document Details

Document Type
Technical Report
Publication Date
May 01, 1971
Accession Number
AD0887506

Entities

People

  • Edward D. Mcdowell Jr
  • Walter T. Jarrett

Organizations

  • Air Force Test Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Control Surfaces
  • Air Traffic Control Systems
  • Aircrafts
  • Control Surfaces
  • Control Systems
  • Flight Control Systems
  • Test And Evaluation
  • Trim Tabs

Readers

  • Aerospace Engineering
  • Aviation Science / Aeronautics.
  • Wetland-Land-Environmental Management.