Experimental Measurements in the Turbulent Boundary Layer of a Yawed, Spinning Ogive-Cylinder Body of Revolution at Mach 3.0. Part 2. Data Tabulation

Abstract

This report presents a tabulation of data for the experiment which is fully described in Part I. Experiment and Data Analysis. The data consist of turbulent boundary layer profile characteristics and wall shear stress for a yawed, spinning slender body of revolution at Mach 3 for angles of attack up to 6.3 degrees. The data tabulations are presented in a format which facilitates their use for comparison to theoretical computations.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1978
Accession Number
ADA053458

Entities

People

  • Lyle D. Kayser
  • Walter B. Sturek

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • C4I
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Artificial Intelligence
  • Bodies
  • Boundary Layer
  • Coordinate Systems
  • Dead Reckoning
  • Geometry
  • Inertial Navigation
  • Layers
  • Mach Number
  • Measurement
  • Plastic Explosives
  • Slender Bodies
  • Static Pressure
  • Three Dimensional
  • Tin
  • Turbulent Boundary Layer
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Fluid Dynamics.