WorldCat Identities

Deriugin, V.

Overview
Works: 5 works in 9 publications in 2 languages and 26 library holdings
Genres: Drama 
Roles: Director
Classifications: TL521.3.C6,
Publication Timeline
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Most widely held works by V Deriugin
Thermal-structural combined loads design criteria study( Book )

5 editions published in 1972 in English and held by 21 WorldCat member libraries worldwide

A study was conducted to determine methodology for combining thermal structural loads and assessing the effects of the combined loads on the design of a thermal protection system and a hot structure of a high cross range delta wing space shuttle orbiter vehicle. The study presents guidelines for establishing a basis for predicting thermal and pressure environments and for determining limit and ultimate design loads on the vehicle during reentry. Limit trajectories were determined by using dispersions on a representative nominal mission and system parameters expected during the life of the vehicle. Nine chosen locations on the vehicle surface having TPS or hot structures were examined, and weight sensitivity analyses were performed for each location
Fluid flow and heat transfer in high-temperature porous matrices for transpiration cooling( Book )

1 edition published in 1966 in English and held by 1 WorldCat member library worldwide

A detailed study of fluid flow and heat transfer characteristics in porous matrices has been performed. Refined prediction methods for pressure and temperature distribution in porous matrices have been developed to include the effects of gas conduction, internal heat sources, chemical reaction, non-steady state flows and slip flow. The show system feasibility, a high-temperature multilayer matrix system has been developed. Six specimens, one inch in diameter, were fabricated and tested in an oxyacetylene flame with and without transpiration cooling. Some tests were performed under a cold wall heat flux of 235 Btu/ft sq-sec. It was found that the specimens can withstand a surface temperature of over 3600 F for a period of 30 minutes. Thus, it has been demonstrated that a transpiration cooled thermal protection system may be developed for space vehicle applications. (Author)
Investigation of fluid flow and heat transfer in porous matrices for transpiration cooling( Book )

1 edition published in 1966 in English and held by 1 WorldCat member library worldwide

An investigation was conducted to determine the heat transfer and fluid flow characteristics in porous matrices for transpiration cooling. Governing differential equations were derived and solved using realistic boundary conditions. Parameters governing the resulting temperature and pressure distributions in porous matrices were identified. Geometry, transient, and dissociation effects on temperature and pressure distributions were determined. Fluid flow and heat transfer characteristics in two-phase flows and multilayer matrices were also analyzed. Experimentally, 301 test runs were performed to measure the temperature distribution and pressure drops across the porous matrices using air, nitrogen, helium, and water as collants. Satisfactory agreement between calculated and measured temperature profiles was obtained. Information on permeability of porous matrices was derived. Good correlation was accomplished for viscous permeability as a function of porosity. (Author)
Beg ot smerti : boevik( Visual )

1 edition published in 1997 in Russian and held by 0 WorldCat member libraries worldwide

Transpiration Cooling System Development for Reentry Vehicles( )

1 edition published in 1968 in English and held by 0 WorldCat member libraries worldwide

This report describes the design, fabrication, and test of a transpiration system test panel module for reentry vehicles. The transpiration system was designed with the objectives of light weight, reusability, minimum refurbishing cost, and mission flexibility. The module development program consisted of four phases: materials, component analysis and development, fabrication of hardware, and test of the module in a plasma facility. This study demonstrated the feasibility of a transpiration system for reentry vehicles
 
Audience Level
0
Audience Level
1
  Kids General Special  
Audience level: 0.75 (from 0.73 for Thermal-st ... to 1.00 for Fluid flow ...)

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