Modeling of Jet Vane Heat-Transfer Characteristics and Simulation of Thermal Response

Abstract

The development of a dynamic computational model capable of predicting, with the requisite design certainty, the transient thermal response of jet vane thrust control systems has been undertaken. The modeling and simulation procedures utilized are based on the concept that the thermal processes associated with jet vane operation can be put into a transfer function form commonly found in the discipline of automatic controls. Well established system identification methods are employed to formulate and verify the relationships between the various gains and frequencies of the transfer function model and experimental data. Keywords: Dynamic systems modeling; Modeling; Model simulation; Thermal response; Parametric system identification; Theses.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1988
Accession Number
ADA199850

Entities

People

  • Mark A. Hatzenbuehler

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Computers
  • Control Systems
  • Fluid Mechanics
  • Heat Capacity
  • Heat Transfer
  • Language
  • Mach Number
  • Mechanical Engineering
  • Models
  • Prandtl Number
  • Rocket Engines
  • Stagnation Point
  • Stagnation Temperature

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation
  • Systems Analysis and Design