Accession Number:

ADA416808

Title:

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

Descriptive Note:

Final rept. 1 Jun 1996-31 Dec 1998

Corporate Author:

CSA ENGINEERING INC PALO ALTO CA

Personal Author(s):

Report Date:

1999-01-01

Pagination or Media Count:

1119.0

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.

Subject Categories:

  • Aerodynamics
  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE