Application of Practical Hydrodynamics to Airship Design.

Abstract

The design of a large high-speed airship is primarily a structural problem, in which the most important stresses are those due, directly or indirectly, to aerodynamic forces on the surface of the hull. The force on any small element of the surface is most conveniently divided into two components, respectively tangent and normal to the surface. The tangent or skin-friction forces are so small per unit area that they are structurally almost negligible compared with the normal forces; yet their total integrated resultant is responsible for almost the entire drag of the hull, whereas the normal components of pressure are so nearly balanced over a good hull that their net resultant is practically zero. The interreaction of these very substantial forces is, of course, through the medium of stresses in the hull, and in combination with fin and inertia forces they are essential not only from a structural standpoint but also in the consideration of stability and control. The distribution of velocity and skin friction can also be indirectly determined from the normal force distribution. An accurate determination of the latter and its effects is therefore of the very first importance.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1931
Accession Number
ADA301035

Entities

People

  • Ralph H. Upson
  • W. A. Klikoff

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aeronautics
  • Aircrafts
  • Boundary Layer
  • Control Surfaces
  • Fineness Ratio
  • Hydrodynamics
  • Mechanical Engineering
  • Navy
  • Pressure Distribution
  • Reynolds Number
  • Skin Friction
  • Skull
  • United States
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Marine Hydrodynamics
  • Systems Analysis and Design