AN Analytical Study of a Boundary Layer TVC Nozzle Concept

Abstract

Experimental investigations of the feasibility of directing missile thrust by controlling ambient airflow through ports in overexpanded nozzles have been conducted by the Naval Weapons Center and an NWC-sponsored contractor. Chandler Evans, Inc. The present analytical effort studied boundary-layer thrust vector control (BLTVC) technology with the following specific objectives: (1) Development of analytical or semi-empirical descriptions of the dominant phenomena that characterize the BLTVC flow field; (2) Derivation of similarity parameters that affect BLTVC performance; (3) Development of preliminary guidelines for flight-environment simulation with ground experiments; and (4) Generation of design charts that would be useful for BLTVC performance evaluation. The results of the study include identification of areas that require investigation in order to establish a design suitable for mission applications.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1976
Accession Number
ADB010287

Entities

People

  • H. H. Tang
  • J. Xerikos
  • W. A. Anderson

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Coordinate Systems
  • Creep
  • Energy Transfer
  • Flow Fields
  • Hot Gases
  • Inviscid Flow
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Physical Properties
  • Pressure Distribution
  • Reynolds Number
  • Test And Evaluation
  • Turbulent Flow
  • Turbulent Mixing

Readers

  • Combustion and Flow Dynamics.
  • Military Training and Readiness Simulation
  • Theoretical Analysis.