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1 edition of Modeling transient thermal behavior in a thrust vector control jet vane found in the catalog.

Modeling transient thermal behavior in a thrust vector control jet vane

Margaret Mary Reno

Modeling transient thermal behavior in a thrust vector control jet vane

by Margaret Mary Reno

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  • 34 Currently reading

Published by Naval Postgraduate School, Available from the National Technical Information Service in Monterey, Calif, Springfield, Va .
Written in English


Edition Notes

ContributionsNunn, R. H. (Robert H.)
The Physical Object
Pagination42 p.
Number of Pages42
ID Numbers
Open LibraryOL25472681M

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. Analysis of the transient behavior and equilibration of the combustion chamber pressure, the stability of the combustion chamber pressure, and the effects of erosive burning is presented. Solid rocket performance characteristics, dual thrust solid rockets, rocket motor casings, and transient operation are .

CFD simulation of a jet vane thrust vector control system R. H. Vaivads, J. E. D. Gauthier, R Farinaccio Transonic wind design by inverse optimization using MOGA S. Obayashi, S. Takahashi, I. Fejtek Computation of the effect of a leading edge glaze ice accretion on finite wing aerodynamics J. Etele, I. Fejtek Thrust vector envelope for three and four vanes. Single-vane deflections at military power and nozzle pressure ratio = 2. Three-and four-vane thrust vectoring control system arrangements.

This paper describes the modeling and validation procedure of a single shaft turbojet engine. The model aim is to provide detailed predictions of the flow’s properties at nozzle outlet. Those predictions will be used to design a thrust vectoring system for the engine, and the flight dynamics control . Mathematical model of the human thermal system, which has been greatly Control volume: Thermal diffusivity a = r Cp k: Thermal expansion coefficients the study of simulating human thermal behavior is moving towards more and more precise methods. In the areas of aerospace.


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Modeling transient thermal behavior in a thrust vector control jet vane by Margaret Mary Reno Download PDF EPUB FB2

Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection Modeling transient thermal behavior in a thrust vector control jet vane. An attempt was made to model the transient thermal response of jet vanes used for thrust control. A simple computer model based on lumped capacitance methods using boundary layer convection and stagnation point heating as thermal inputs appeared to adequately predict temperatures for a quarter- scale model.

An attempt was made to model the transient thermal response of jet vanes used for thrust control. A simple computer model based on lumped capacitance methods using boundary layer convection and stagnation point heating as thermal inputs appeared to adequately predict temperatures for a quarter-scale model.

To submit an update or takedown request for this paper, please submit an Update/Correction/Removal : Margaret Mary. Reno. The report presents heat transfer modeling of Thrust Vector control systems using the PHOENICS computer code. Simple two-dimensional wedged blunt bodies have been examined in supersonic cold flow.

Although some state of the art modeling approaches have been presented for simulating the thermal behavior, these have focused on thermally stable conditions.

In this work, an instrumented turbocharger was operated on a liter diesel engine and in parallel a one-dimensional lumped capacity thermal model was by: Modelling of Transient Behaviour in a Francis Turbine Power Plant Tzuu Bin Ng, G.J.

Walker and J.E. Sargison School of Engineering The University of Tasmania, Hobart, TAS, AUSTRALIA Abstract This paper presents a nonlinear mathematical model of the Francis turbine for a single-machine hydroelectric power Size: KB.

T1 - Analysis and modeling of the transient thermal behavior of automotive turbochargers. AU - Burke, R D. PY - /10/1. Y1 - /10/1. N2 - Turbochargers are a key technology to deliver fuel consumption reductions on future internal combustion by: T1 - Analysis and modelling of the transient thermal behaviour of automotive turbochargers.

AU - Burke, R D. N1 - Paper number: ICEF PY - /10/ Y1 - /10/ N2 - Turbochargers are a key technology to deliver fuel consumption reductions on future internal combustion by: 3. a comprehensive model that includes all the influential factors while it is feasible for being implemented in the ECUs, was aimed for this work.

Therefore, the chemical investigating of the problem leaded to propose a first kinetic model and its thermal analysis caused modelling the oil thermal behaviour. According to the thrust vector control requirements of fast turn of the missile vertical launching, this design carries out the force analysis of the jet vane which is in the high temperature and high speed jet stream, and calculates the normal force which is generated by the vane, thus calculates the area of the jet : Liu Min Wang, Bo Mo.

From the results of transient thermal 3D CFD simulations of the load case ‘Cooldown’ a model for the respective parameters is derived by means of a Linear Time-Invariant System (LTI) approach. These parameters then serve as transient boundary conditions in an independently running, predictive thermal cabin : David Klemm, Wolfgang Rößner, Nils Widdecke, Jochen Wiedemann.

Thrust-Vector Characteristics of Jet Vanes Arranged in X-Formation Within a Shroud. Transformation model of thrust-vectoring using RBF neural network. Research on the thrust vector control via jet vane in rapid turning of vertical by: The potential flow around a jet vane and the transient heat conduction in it were simulated while the heat flux on a vane surface was calculated with the analytic method for the thermal boundary.

Jet vane thrust vector control - A design effort. Thrust-Vector Characteristics of Jet Vanes Arranged in X-Formation Within a Shroud. Hong-Gye Sung and Yong-Seok Hwang; Journal of Propulsion and Power Vol. 20, No. 3 May BEM model of ablation characteristics of a thrust vector control vane.

The transient thermal distribution in the turbine valve is displayed in terms of instantaneous thermal distribution on the xy plane in four representative instances in Fig.

The fluid temperature and the solid temperature corresponding to the conjugate heat transfer are plotted by: 1. tively few of them deal with the transient thermal modeling of microelectronicdevices [10], [11].

However, with growing a number of applications, the transient thermal behavior of in-tegrated devices remains a critical issue. Since this phenome-non strongly affects the maximum dissipated power it isvery.

Design and development of jet vane based thrust vector control system for a solid rocket motor Prediction of residual thrust for high altitude solid rocket motors due to out gassing from thermal insulation.

Srinivasan, R Numerical simulation of soot and gas radiation effects on transient combustion of spherical droplets. This video shows how to create a transient thermal analysis in Autodesk Simulation Mechanical.

It also shows how to use nodal temperature data from the analsysis as input for a thermal. A further examination of Figure 2a indicates that there are alternating regions of different transient behavior: 1) small thickness and large temperature rise (TIMs and heat-sink-to- air thermal resistance) and 2) larger thickness and small temperature rise across them (die, lid.

Živković, S. @., et al.: Experimental and Simulation Testing of Thermal Loading in THERMAL SCIENCE, YearVol. 20, Suppl. 1, pp. SS S EXPERIMENTAL AND SIMULATION TESTING OF THERMAL LOADING IN THE JET TABS OF A THRUST VECTOR CONTROL SYSTEM by Saša @. ŽIVKOVI]a*, Mom~ilo M. MILINOVI]b, Predrag Lj. STEFANOVI]c.jet engine must remain in a vertical orientation to not contribute to lateral motions.

To thisend,athrustvectoringmechanismwasdesignedandbuiltthat,togetherwithasuite of sensors and a closed loop control algorithm, enables precise orientation control of the jet engine. Detailed designs for the thrust vectoring mechanisms and control avionics areCited by: 6.

Heat transfer modeling of jet vane Thrust Vector Control (TVC)--Systems. Item Preview remove-circle Share or Embed This Item.

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