A Structural Weight Estimation Program (SWEEP) for Aircraft. Volume VI - Wing and Empennage Module. Appendix E: Program Listings, Overlays (8,0), (14, 0), (15,0), (16,0), and (17,0)

Abstract

Three computer programs were written with the objective of predicting the structural weight of aircraft through analytical methods. The first program, the structural weight estimation program (SWEEP), is a completely integrated program including routines for airloads, loads spectra, skin temperatures, material properties, flutter stiffness requirements, fatigue life, structural sizing, and for weight estimation of each of the major aircraft structural components. This volume (volume 6) contains the methods and program description for the wing and empennage module of SWEEP. Program listings and flow charts are included in the appendix to this volume.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1974
Accession Number
ADA002862

Entities

People

  • G. Hayase

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Composite Materials
  • Computer Programs
  • Control Surfaces
  • Data Processing
  • Geometry
  • Government Procurement
  • Leading Edges
  • Lifting Surfaces
  • Mass Storage
  • Materials
  • Stiffness
  • Structural Components
  • Surface Analysis
  • Surfaces
  • Trailing Edges

Readers

  • Aerodynamics.
  • Computer Science.
  • Structural Health Monitoring of Composite Structures.