PRESSURE AND HEAT TRANSFER MEASUREMENTS FOR MACH 8 FLOWS OVER A BLUNT PYRAMIDAL CONFIGURATION WITH AERODYNAMIC CONTROLS. PART 3: HEAT TRANSFER DATA FOR DELTA WING SURFACE

Abstract

The report presents heat transfer data obtained in the AEDC 50-inch Mach 8 tunnel on the lower surface of a blunt pyramidal configuration having remotely controlled trailing edge flaps.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1964
Accession Number
AD0601804

Entities

People

  • Louis G. Kaufman Ii.

Organizations

  • Grumman

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Heating
  • Air Force
  • Delta Wings
  • Engineering
  • Experimental Data
  • Flight
  • Flow Separation
  • Fluid Dynamics
  • Free Stream
  • Heat Transfer
  • Hypersonic Flow
  • Instrumentation
  • Leading Edges
  • Measurement
  • Shock Tunnels
  • Sideslip

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.