Heated Wing Analysis Method Formulas and Details

Abstract

A method for analyzing heated thin wings was developed under a Grumman Advanced Development Program and is reported in the paper, "A Matrix Force Method for Analyzing Heated Wings, Including Large Deflections". This paper was presented at the symposium "Structural Dynamics of High Speed Flight", sponsored by the Aerospace Industries Association and The Office of Naval Research in Los Angeles, California, April 24-26, 1961. The present report contains some details on certain aspects of the method, which were of necessity omitted from the paper. Several examples illustrating the application of the method are contained in the paper and might be referred to while this report is being read. This report and Refs. 2, 3 and 4 document the Grumman matrix force method of redundant structure analysis as developed to date. The same notation is used throughout these references.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
ADA377257

Entities

People

  • I. W. Jones

Organizations

  • Grumman

Tags

DTIC Thesaurus Topics

  • Aerospace Industry
  • Aircrafts
  • Axial Loads
  • Buckling
  • Climate Change
  • Corporations
  • Deflection
  • Displacement
  • Engineering
  • Equations
  • Load Distribution
  • Military Research
  • Resilience
  • Spars
  • Stresses
  • Thermal Stresses
  • Thin Wings

Readers

  • Aerodynamics/Aeronautics.
  • Regression Analysis.
  • Technical Research and Report Writing.

Technology Areas

  • Space