Some Measurements of the Magnus Characteristics on a Magnetically- Suspended 5-Caliber Ogive Cylinder

Abstract

The Magnus side force and yawing moment on a spinning 5-caliber ogive cylinder have been measured using the magnetic suspension and balance system at this laboratory. Data are reported at M = .27 to .43 and Re = 100,000 to 1,200, 000 at non-dimensional spin rate, PD/2V between 0 and 0.14. The Magnus side force is found to undergo reversal from its classical direction at angles of attack below 5 deg and Re = 770,000. Above 7 deg angle of attack the side force is in the classical direction and in agreement with the data in the literature. The reverse Magnus force is a maximum at 2 deg angle of attack. The peak value is reduced by increase in Reynolds number, by artificially induced boundary layer transition and by the presence of a support sting. At angles of 7 and 9 deg both artificial roughness and a support sting increase the size of the classical Magnus force. Results are compared with other reported data.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1977
Accession Number
ADA035861

Entities

People

  • C. W. Haldeman
  • E. E. Covert
  • E. P. Birtwell
  • J. B. Coffin

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Ground and Sea Platforms
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Agreements
  • Boundary Layer
  • Boundary Layer Flow
  • Boundary Layer Transition
  • Computational Fluid Dynamics
  • Cross Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Information Processing
  • Jet Propulsion
  • Measurement
  • Reynolds Number
  • Three Dimensional
  • Turbulent Boundary Layer
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.