Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination.

Abstract

A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. Volume V presents the tabulated flow-field data for 6-percent thick wing model.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1977
Accession Number
ADA062274

Entities

People

  • Michael J. Hemsch
  • Stanley C. Perkins Jr.
  • Stephen S. Stahara

Organizations

  • Nielsen Engineering & Research (United States)

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Artificial Intelligence
  • Automatic Identification Systems
  • Capillary Electrophoresis
  • Dynamic Pressure
  • Engineering
  • Flow
  • Flow Fields
  • Instruction Set Architecture
  • Mach Number
  • Measurement
  • Microarchitecture
  • Network Protocols
  • Plastic Explosives
  • Self Assembly
  • Static Pressure
  • Thick Wings
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics