AN EXPERIMENTAL INVESTIGATION OF LAMINAR HYPERSONIC CAVITY FLOWS

Abstract

An experimental investigation was made of the recovery factor and heat-transfer distributions on a set of cone-models incorporating annular cavities. This study is the second part of a two-part program. The first section contained measurements of the pressure distributions. The results show that the recovery factor in laminar, hypersonic cavity flow is almost constant within the cavity and downstream of reattachment, and is very close to the laminar attached-flow value. In the immediate vicinity of reattachment, the recovery factor is slightly higher than this value (less than 5%). The lowest values of the heat-transfer coefficient are found on the cavity floors, where a minimum of about 10 to 20% of the attached-flow value is reached. The highest values of the heat-transfer coefficient are in the immediate vicinity of reattachment. An average reattachment heat transfer coefficient of about three times the basic cone heat-transfer coefficient was measured on one cavity model.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0430710

Entities

People

  • K. M. Nicoll

Organizations

  • Princeton University

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Fluid Dynamics
  • Fluid Flow
  • Government Procurement
  • Heat Capacity
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Measurement
  • Physics Laboratories
  • Pressure Distribution
  • Reynolds Number
  • Stagnation Pressure
  • Temperature Gradients
  • Turbulent Mixing
  • United States

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Marine Propulsion Engineering and Naval Architecture

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow