Statistical Methods and Their Application to Establishing Flight Maneuver Loads Design Criteria for Fighter Aircraft.

Abstract

The report provides statistical methods for use in establishing positive maneuver loads design criteria for fighter aircraft. These methods are applied to counting accelerometer data and comparisons between operational loads data and military specifications are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0735472

Entities

People

  • Thomas A. De Fiore
  • William C. Stewart

Organizations

  • Naval Air Warfare Center Warminster

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accelerometers
  • Aircrafts
  • Design Criteria
  • Fighter Aircraft
  • Flight
  • Flight Maneuvers
  • Maneuvers
  • Military Aircraft
  • Specifications
  • Standards

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Marine Hydrodynamics
  • Regression Analysis.