Time Histories of Loads and Deformation on a B-45A Airplane in Two Aileron Rolls

Abstract

Loads measured on the horizontal tail, vertical tail, and wing and the aeroelastic distortions of elevators, stabilizers, and fuselage of a B-45A airplane in a right and left roll at a Mach number of 0.60 and an altitude of 15,000 feet are presented. The data are given in time-history form.

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Document Details

Document Type
Technical Report
Publication Date
Nov 08, 1949
Accession Number
ADA800920

Entities

People

  • T. V. Cooney
  • William A. Mcgowan

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airfoils
  • Airplanes
  • Altitude
  • Center Of Gravity
  • Control Surfaces
  • Deflection
  • Electrical Resistance
  • Horizontal Stabilizers
  • Mach Number
  • Measurement
  • Stabilization Systems
  • Strain Gages
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.