Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume IV. Mach Number 1.025 Flow-Field Survey Data for the 4-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. Volume IV presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 1.025.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1977
Accession Number
ADA062273

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

  • Aircrafts
  • Dynamic Pressure
  • Engineering
  • External Stores
  • Flow
  • Flow Fields
  • Free Stream
  • Mach Number
  • Measurement
  • Nomenclature
  • Operating Systems
  • Plastic Explosives
  • Self Assembly
  • Static Pressure
  • Thick Wings
  • Tunnels
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics