A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and without Tail Fins and Wings. Volume 2. Appendixes A through E. Tests Number 1 through 5

Abstract

Volume II contains the tabulated data obtained during Test Number 1 and 2 at AEDC and Tests Number 3, 4, and 5 at NASA Langley Research Center.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1976
Accession Number
ADB010054

Entities

People

  • G. R. Gomillion

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Bending Moments
  • Dynamic Pressure
  • Engineering
  • Engineers
  • Governments
  • Leading Edges
  • Molecular Orbital Theory
  • Operating Systems
  • Slender Bodies
  • Static Pressure
  • Systems Engineering
  • Test And Evaluation
  • United States
  • Unmanned Ground Systems
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics