Nose Pressure Fluctuations for a Finite-Thickness Symmetric Body Penetrating a Sinusoidal Transverse Velocity Field

Abstract

The effects of the transverse component of velocity fluctuations on nominal stagnation point (NSP) pressure fluctuations are analyzed for a finite- thickness symmetric body penetrating into a turbulent flow. The analysis is idealized to the case of a two-dimensional symmetric airfoil-like profile. The results are given in analytical form.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
AD0782035

Entities

People

  • Frank Lane

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accounting
  • Airfoils
  • Equations
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Integral Equations
  • Integrals
  • Leading Edges
  • Motion
  • Potential Flow
  • Stagnation Point
  • Thickness
  • Thin Wings
  • Trailing Edges
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.