Access the full text.
Sign up today, get DeepDyve free for 14 days.
Loading next page...
/lp/springer-journals/modeling-of-the-thermal-protection-system-based-on-the-thermionic-vsfBWC1s8N
References (36)
-
K. Jensen (2017)
Introduction to the Physics of Electron Emission -
V. Peletskii, V. Voskresenskii (1966)
TANTALUM THERMOPHYSICAL PROPERTIES AT TEMPERATURES ABOVE 1000 DEGREE K. -
A. Yakimov (2018)
Thermal Protection Modeling of Hypersonic Flying Apparatus -
L. Uribarri, E. Allen (2015)
Electron Transpiration Cooling for Hot Aerospace Surfaces -
Kyle Hanquist, I. Boyd (2019)
Plasma Assisted Cooling of Hot Surfaces on Hypersonic VehiclesFrontiers in Physics
-
(2012)
Active thermal protection of structural elements of a high-velocity flying vehicle based on new physical principles during aerodynamic heating, Electronic journal “Trudy MAI, -
A. Yakimov (2018)
Combined Thermal Protection -
(2006)
Software and results of modeling of thermionic systems -
V. Zinchenko, K. Efimov, A. Yakimov (2011)
Calculation of the characteristics of conjugate heat-mass exchange under spatial flow of a blunt body with the use of a combined heat protection systemHigh Temperature, 49
-
(2001)
Kalandarishvili, Working Processes in Thermionic Converters of Nuclear Power Facilities -
(1971)
Simple empirical formula for electron emission from metal surfaces covered by cesium. Direct conversion of thermal energy to electric energy and fuel cells -
K. Efimov, V. Ovchinnikov, A. Yakimov (2017)
Rotation Influence on Heat Transfer at Supersonic Flow Around a Blunted BodyAIAA Journal, 56
-
(2009)
Thermionic method of protection of flying vehicle elements against aerodynamic heating, Patent No. 2404087 RF, MPK 51 B64C 1/38, В64G 1/50, Paten holder Baltic State Technical University "Voenmekh -
Kyle Hanquist, K. Hara, I. Boyd (2017)
Detailed modeling of electron emission for transpiration cooling of hypersonic vehiclesJournal of Applied Physics, 121
-
(1968)
Thermophysical Properties of Materials in Nuclear Power Engineering -
(1975)
Empirical method for calculating Volt-Ampere characteristics of TECs, Tech -
(1969)
Yuditskii, Generalized calculation of currentvoltage characteristics and temperature fields of thermionic converters on the basis of testing a TC -
Kyle Hanquist, I. Boyd (2017)
Computational analysis of electron transpiration cooling for hypersonic vehicles -
N. Vargaftik, Yu. Vinogradov, V. Yargin (1983)
Handbook of Physical Properties of Liquids and Gases -
(2000)
Methods and Tools of Experimental Investigations and Reactor Testing of Thermionic Electric Generating Assemblies -
K. Efimov, V. Ovchinnikov, A. Yakimov (2017)
Mathematical modeling of rotation effects on conjugate heat and mass transfer at a high-enthalpy flow around a spherically blunted cone at incidenceThermophysics and Aeromechanics, 24
-
N. Bezverkhnii, S. Bobashev, A. Kolychev, N. Monakhov, S. Ponyaev, V. Sakharov (2019)
Study of the Effect of Electron Cooling: Overview of the Current StateTechnical Physics, 64
-
Kyle Hanquist, H. Alkandry, I. Boyd (2017)
Evaluation of Computational Modeling of Electron Transpiration Cooling at High EnthalpiesJournal of Thermophysics and Heat Transfer, 31
-
B. Zemlyanskii, G. Stepanov (1981)
Calculation of heat transfer accompanying hypersonic three-dimensional flow of air over slender blunt-nosed conesFluid Dynamics, 16
-
Yu. Skorik (1975)
Foundations of thermionic energy conversionSoviet Atomic Energy, 38
-
F. Rufeh, D. Lieb (1969)
OUTPUT CHARACTERISTICS OF A VAPOR-DEPOSITED TUNGSTEN EMITTER AND A MOLYBDENUM COLLECTOR. -
(1981)
Algorithm for calculating thermionic electric generating assemblies -
(1990)
Limiting output characteristics of TC, Abstracts of Intern. Conf -
Ye.G. D'yakonov (1964)
Introduction to the theory of difference schemes -
(1968)
Hypersonic Flow around Blunted Cones with Allowance for Equilibrium Physical and Chemical Transformations -
(1982)
Method for calculating batteries of thermionic converters, Izv -
(2011)
Mathematical and Physical Modeling of Thermal Protection -
N. Rasor, C. Warner (1964)
Correlation of Emission Processes for Adsorbed Alkali Films on Metal SurfacesJournal of Applied Physics, 35
-
(1974)
Emel'yanov, Fundamentals of Thermionic Conversion of Energy -
(2014)
Development of a technique for calculating the multielement thermionic thermal protection for hypersonic flying vehicles, Electronic journal “Trudy MAI, -
V. Bodryakov (2013)
Heat capacity of solid tantalum: Self-consistent calculationHigh Temperature, 51
- Publisher
- Springer Journals
- Copyright
- Copyright © V.P. Zimin, K.N. Efimov, V.A. Kernozhitskii, A.V. Kolychev, V.A. Ovchinnikov, and A.S. Yakimov 2020
- ISSN
- 0869-8643
- eISSN
- 1531-8699
- DOI
- 10.1134/S0869864320020055
- Publisher site
- See Article on Publisher Site
Abstract
The mathematical model of unsteady heat transfer in the thermionic thermal protection system during high-enthalpy heating is studied numerically. The effect of evaporation of electrons from the emitter surface on reduction of the temperature of the multilayered shell of the thermionic thermal protection system is demonstrated. The influence of some heat transfer agents in the composite shell on the regimes of heat transfer in the body is considered. Qualitative agreement of the calculated results with available data is obtained.
Journal
Thermophysics and Aeromechanics – Springer Journals
Published: Mar 2, 2020