An Experimental Investigation of Tangential Blowing to Reduce Buffet Response of the Vertical Tails of an F-15 Wind Tunnel Model. Volume 3 - Oscillatory Pressure Data

Abstract

This is Volume 3 of AN EXPERIMENTAL INVESTIGATION OF TANGENTIAL BLOWING TO REDUCE BUFFET RESPONSE OF THE VERTICAL TAILS OF AN F-15 WIND TUNNEL MODEL. This volume presents the detailed CSD graphs, in magnitude and phase plots, and gives summary tables of rms values of the magnitudes from those graphs. To aid with the comprehension of this data, figures from volume 1 showing the model, setup, and model instrumentation are repeated here. The reader will most likely have to refer to volume 1 for added tie-in.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1999
Accession Number
ADA416808

Entities

People

  • Elijah W. Turner
  • Marty A. Ferman

Tags

Communities of Interest

  • Air Platforms
  • C4I

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Aircrafts
  • Engineering
  • Governments
  • Instrumentation
  • Intellectual Property
  • Military Research
  • Models
  • Pressure Measurement
  • Stereolithography
  • Three Dimensional
  • Unsteady Aerodynamics
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.