AERODYNAMIC CHARACTERISTICS OF PROPOSED SNAP-29 FUEL BLOCK CONFIGURATIONS AT MACH NUMBER 8.

Abstract

Selected static-stability test results of five proposed SNAP-29 fuel block configurations are presented. Test configuration changes were made by varying the edge shape of the basic flat plate fuel block. Tests of 0.25- and 0. 50-scale models were conducted at a nominal Mach number of 8, Reynolds number based on model length of 0.6 x to the 6th power, and angles of attack from 0 to 90 deg. Results of model support interference studies employing oil flow, pressure distribution, and image-type force data techniques are presented.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1967
Accession Number
AD0813438

Entities

People

  • R. H. Burt
  • W. R. Martindale

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Contractors
  • Contracts
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Government (Foreign)
  • Government Procurement
  • Governments
  • Instrumentation
  • Mach Number
  • Models
  • Pressure Distribution
  • Reynolds Number
  • Scale Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Missile Defense Systems.