Accession Number:

ADA409895

Title:

F-15 8.33-Percent Model Internozzle Dynamic Pressure Environment

Descriptive Note:

Final rept. 1-31 May 1986

Corporate Author:

AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH AIR VEHICLES DIRECTORATE

Report Date:

1986-05-01

Pagination or Media Count:

54.0

Abstract:

The F-15 Strategic Programs Office ASDTAF requested the Structural Vibration and Acoustics Branch to record and analyze data from a wind tunnel test on an 8.33-percent model F-15 aircraft. The objective was to assess the effect various model configurations had on the aeroacoustic loads around the aft nozzle region.

Subject Categories:

  • Aerodynamics
  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE