F-15 8.33-Percent Model Internozzle Dynamic Pressure Environment

Abstract

The F-15 Strategic Programs Office (ASD/TAF) 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.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1986
Accession Number
ADA409895

Entities

People

  • C. J. Otto
  • D. L. Banaszak
  • G. L. Plzak
  • L. L. Shaw

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acoustics
  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Aircrafts
  • Data Acquisition
  • Dynamic Pressure
  • Environment
  • Frequency
  • Government Procurement
  • Governments
  • Mach Number
  • Mechanics
  • Structural Mechanics
  • Test Facilities
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.
  • Defense Acquisition Program Management