Evaluation of SAGMI and HAST Airloads at the F-4C Centerline Carriage Position for Subsonic and Transonic Mach Numbers

Abstract

A wind tunnel investigation was conducted to determine the airloads on the SAGMI and HAST vehicles at the F-4C centerline carriage position. In the process of obtaining these loads, a limited amount of sting interference data on the SAGMI vehicle was obtained. Force and moment data were recorded at Mach numbers from 0.50 to 1.20 for angles of attack from -4 to 12 deg and angles of sideslip from -8 to 8 deg.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1972
Accession Number
AD0893134

Entities

People

  • Richard W. Butler

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Base Pressure
  • Carriages
  • Coefficients
  • Dynamic Pressure
  • Flow
  • Flow Fields
  • Free Stream
  • Instrumentation
  • Mach Number
  • Measurement
  • Research Facilities
  • Sideslip
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.