Data Report for a Test Program to Study Transonic Flow Fields About Wing-Body/Pylon/Store Combinations. Volume II. Flow Field Survey Data for Configurations 21 and 22.

Abstract

This volume of the data report presents the flow-field survey data for configurations 21 and 22 at Mach numbers M1 = 0.925, M2 = 0.950, and M3 = 1.05 and angles of attack alpha = 0 deg, 2 deg, and 5 deg. The data were obtained in the 4T Wind Tunnel at Arnold Engineering and Development Center. The tests were performed at a nominal Reynolds number per foot of 3.0 million.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1978
Accession Number
ADA077183

Entities

People

  • A. J. Crisalli
  • S. S. Stahara

Organizations

  • Nielsen Engineering & Research (United States)

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Birds
  • Coordinate Systems
  • Flow Fields
  • Free Stream
  • Intellectual Property
  • Mach Number
  • Network Protocols
  • Operating Systems
  • Plastic Explosives
  • Pressure Distribution
  • Pressure Measurement
  • Silicon Carbide
  • Software In The Loop
  • Static Pressure
  • Tank Guns
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics