Главная Новые поступления Описание Шлюз Z39.50

Базы данных


Труды сотрудников Института теплофизики УрО РАН - результаты поиска

Вид поиска

Область поиска
в найденном
 Найдено в других БД:Каталог книг и продолжающихся изданий (436)Каталог диссертаций и авторефератов диссертаций УрО РАН (11)Каталог препринтов УрО РАН (1975 г. - ) (4)Изобретения уральских ученых (1)Интеллектуальная собственность (статьи из периодики) (6)Нанотехнологии (11)История Урала (1)Книжная коллекция Шубиных (1)Труды Института высокотемпературной электрохимии УрО РАН (92)Труды Института истории и археологии УрО РАН (39)Труды сотрудников Института горного дела УрО РАН (10)Труды сотрудников Института органического синтеза УрО РАН (81)Труды сотрудников Института химии твердого тела УрО РАН (79)Расплавы (101)Публикации Черешнева В.А. (30)Публикации Чарушина В.Н. (36)Каталог библиотеки ИЭРиЖ УрО РАН (20)
Формат представления найденных документов:
полный информационныйкраткий
Отсортировать найденные документы по:
авторузаглавиюгоду изданиятипу документа
Поисковый запрос: (<.>K=Th<.>)
Общее количество найденных документов : 36
Показаны документы с 1 по 20
 1-20    21-36 
1.

Вид документа :
Шифр издания : 53/T 44
Автор(ы) : Bienert W. B., Wolf D. A., Nikitkin M. N., Maydanik Yu. F., Fershtater Y. G., Vershinin S. V., Gottschlich J. M.
Заглавие : The proof-of-feasibility of multiple evaporator loop heat pipes
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol.400. - С. 393-398
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --thermal control --multiple thermal interface
Аннотация: This paper presents results that demonstrate the proof-of-feasibility of multiple evaporator Loop Heat Pipes (LHP). It was demonstrated that a multiple evaporator LHP can successfully operate as a thermal control system component. A breadboard LHP with multiple evaporators (two) that retained the reliable self starting behavior of the single thermal interface LHP was developed. Program efforts were concentrated on a two pump system and investigated the performance of the dual evaporator LHP. Analytical predictons and experimental test data are compared, and important issues are discussed that will be a baseline for continued development of multiple thermal interface LHPs. All of the conclusions are based on test results, analytic modeling and the correlation of the two. Although a mathematical model that predicts the multiple evaporator LHP behavior was developed, the primary focus of the program was the development, fabrication, and test of a breadboard multi-evaporator LHP. The program clearly demonstrated that multi-evaporator LHPs are feasible and merit further development as a viable thermal control components
Найти похожие

2.

Вид документа :
Шифр издания : 53/T 44
Автор(ы) : Bienert W. B., Wolf D. A., Nikitkin M. N., Maydanik Yu. F., Fershtater Y. G., Vershinin S. V., Gottschlich J. M.
Заглавие : The proof-of-feasibility of multiple evaporator loop heat pipes
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol.400. - С. 393-398
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --thermal control --multiple thermal interface
Аннотация: This paper presents results that demonstrate the proof-of-feasibility of multiple evaporator Loop Heat Pipes (LHP). It was demonstrated that a multiple evaporator LHP can successfully operate as a thermal control system component. A breadboard LHP with multiple evaporators (two) that retained the reliable self starting behavior of the single thermal interface LHP was developed. Program efforts were concentrated on a two pump system and investigated the performance of the dual evaporator LHP. Analytical predictons and experimental test data are compared, and important issues are discussed that will be a baseline for continued development of multiple thermal interface LHPs. All of the conclusions are based on test results, analytic modeling and the correlation of the two. Although a mathematical model that predicts the multiple evaporator LHP behavior was developed, the primary focus of the program was the development, fabrication, and test of a breadboard multi-evaporator LHP. The program clearly demonstrated that multi-evaporator LHPs are feasible and merit further development as a viable thermal control components
Найти похожие

3.

Вид документа :
Шифр издания : 53/T 44
Автор(ы) : Orlov A. A., Goncharov K., Kotiarov E. Y., Tyklina T. A., Ustinov S. N., Maydanik Yu. F.
Заглавие : The loop heat pipe experiment on board the GRANAT spacecraft
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol. 400. - С. 341-353
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --alyona--experimental system
Аннотация: Results of the most durable Russian on-orbit experiment with the Loop Heat Pipe are analyzed in present paper. All telemetry data on temperature measurements obtained from the experimental system ALYONA during its performance period from 1989 till 1996 are compared. Estimation of the LHP operation ability during the whole period mentioned above and determination of the calculated value of transferred heat power were executed with taking into account the boundary conditions characterizing the operation mode of the experimental system ALYONA. Some results of on-ground testing, real characteristics of radiating surfaces coating and, also, the scientific spacecraft GRANAT orientation data were taken into account for analyzing. Necessary information on the Loop Heat Pipe design, used materials, preliminary on-ground testing is presented. Besides this, the information that allows to make a conclusion on the successful Loop Heat Pipe re-starting modes occurring when the spacecraft comes into the shade zone and to judge on the LHP life time is also presented. Documents provided by different LAVOCHKIN ASSOCIATION sen ices and divisions controlling the communication data obtained from the spacecraft were used for this paper preparation
Найти похожие

4.

Вид документа :
Шифр издания : 53/T 44
Автор(ы) : Orlov A. A., Goncharov K., Kotiarov E. Y., Tyklina T. A., Ustinov S. N., Maydanik Yu. F.
Заглавие : The loop heat pipe experiment on board the GRANAT spacecraft
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol. 400. - С. 341-353
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --alyona--experimental system
Аннотация: Results of the most durable Russian on-orbit experiment with the Loop Heat Pipe are analyzed in present paper. All telemetry data on temperature measurements obtained from the experimental system ALYONA during its performance period from 1989 till 1996 are compared. Estimation of the LHP operation ability during the whole period mentioned above and determination of the calculated value of transferred heat power were executed with taking into account the boundary conditions characterizing the operation mode of the experimental system ALYONA. Some results of on-ground testing, real characteristics of radiating surfaces coating and, also, the scientific spacecraft GRANAT orientation data were taken into account for analyzing. Necessary information on the Loop Heat Pipe design, used materials, preliminary on-ground testing is presented. Besides this, the information that allows to make a conclusion on the successful Loop Heat Pipe re-starting modes occurring when the spacecraft comes into the shade zone and to judge on the LHP life time is also presented. Documents provided by different LAVOCHKIN ASSOCIATION sen ices and divisions controlling the communication data obtained from the spacecraft were used for this paper preparation
Найти похожие

5.

Вид документа : Статья из журнала
Шифр издания : 53/S 71
Автор(ы) : Maydanik Yu. F., Fershtater Y. G., Vershinin S. V., Pastukhov V. G., Goncharov K.
Заглавие : Some results of loop heat pipes development, tests and application in engineering
Место публикации : Proceedings of 5th International Heat Pipe Symposium (Melbourne, Australia, Nov. 17-20, 1996). - Melbourne, 1996. - С. 406-412
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): труба контурная--контурная труба--труба тепловая--тепловая труба
Найти похожие

6.

Вид документа : Статья из журнала
Шифр издания : 53/S 71
Автор(ы) : Maydanik Yu. F., Fershtater Y. G., Vershinin S. V., Pastukhov V. G., Goncharov K.
Заглавие : Some results of loop heat pipes development, tests and application in engineering
Место публикации : Proceedings of 5th International Heat Pipe Symposium (Melbourne, Australia, Nov. 17-20, 1996). - Melbourne, 1996. - С. 406-412
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): труба контурная--контурная труба--труба тепловая--тепловая труба
Найти похожие

7.

Вид документа : Статья из журнала
Шифр издания : 53/S 66
Автор(ы) : Skripov V. P.
Заглавие : Phase-change behavior of water in noneguilibrium processes
Место публикации : Proceedings of the 10th International Conference on the Properties of Steam (Moscow, Mir Publishers). - M., 1986. - V. 1. - С. 227-251
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): вода--процесс неравновесный--неравновесные процессы
Найти похожие

8.

Вид документа : Статья из журнала
Шифр издания : 53/S 66
Автор(ы) : Skripov V. P.
Заглавие : Phase-change behavior of water in noneguilibrium processes
Место публикации : Proceedings of the 10th International Conference on the Properties of Steam (Moscow, Mir Publishers). - M., 1986. - V. 1. - С. 227-251
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): вода--процесс неравновесный--неравновесные процессы
Найти похожие

9.

Вид документа : Статья из журнала
Шифр издания : 53/S 66
Автор(ы) : Skokov V. N., Koverda V. P., Bogdanov N. M.
Заглавие : Thermal bistability and nonequilibrium phase transitions in thin HTSC-films under transport current
Место публикации : 14th International Cryogenic Engineering Conference and Cryogenic Materials Conference (Ukraine, Kiev, 1992, 8-12 June). - Kiev, 1992. - С. 135
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): бистабильность термическая--термическая бистабильность--переходы фазовые--фазовые переходы--htsc пленки тонкие--перенос тока--тока перенос--переход неравновесный--неравновесные переходы
Найти похожие

10.

Вид документа : Статья из журнала
Шифр издания : 53/S 66
Автор(ы) : Skokov V. N., Koverda V. P., Bogdanov N. M.
Заглавие : Thermal bistability and nonequilibrium phase transitions in thin HTSC-films under transport current
Место публикации : 14th International Cryogenic Engineering Conference and Cryogenic Materials Conference (Ukraine, Kiev, 1992, 8-12 June). - Kiev, 1992. - С. 135
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): бистабильность термическая--термическая бистабильность--переходы фазовые--фазовые переходы--htsc пленки тонкие--перенос тока--тока перенос--переход неравновесный--неравновесные переходы
Найти похожие

11.

Вид документа :
Шифр издания : 53/P 31
Автор(ы) : Pastukhov V. G., Maydanik Yu. F., Fershtater Y. G.
Заглавие : Adaptation of loop heat pipes to zero-g conditions
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol.400. - С. 385-391
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --heat-transport --thermocapillary phenomena
Аннотация: Loop heat pipes (LHPs) posses a great variety of valuable properties, which make them quite promising for application both on the Earth and in space. Among these are the LHP high heat-transport capacity at an any orientation in the field of mass forces, good mass-and-size parameters and the possibility of an arbitrary configuration of transport lines. At the same time such a drawback of LHPs of the conventional type as the instability of start up and operation in the region of low heat loads reduces their performance. The problem is connected, in a general case, with the unfavourable distribution of the vapor and the liquid phases of the working fluid in the evaporator. There is reason to believe that the LHP operation can also be significantly affected by zero-g conditions, in which the distribution of a working fluid is pre-determined only by the action of surface forces and the thermocapillary phenomena. The paper performs a general analysis of the necessary conditions imposed on the construction of LHP and some designs that contribute to the retention of serviceability in zero-g conditions at low heat loads. It gives the results of laboratory investigations of an adapted ammonia LHP with a heat-transfer capacity up to 2 kWxm
Найти похожие

12.

Вид документа :
Шифр издания : 53/P 31
Автор(ы) : Pastukhov V. G., Maydanik Yu. F., Fershtater Y. G.
Заглавие : Adaptation of loop heat pipes to zero-g conditions
Место публикации : 6th European Symposium on Space Environmental Control Systems: Noordwijk, Netherlands, 20-22 may 1997 . - 1997. - Vol.400. - С. 385-391
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --heat-transport --thermocapillary phenomena
Аннотация: Loop heat pipes (LHPs) posses a great variety of valuable properties, which make them quite promising for application both on the Earth and in space. Among these are the LHP high heat-transport capacity at an any orientation in the field of mass forces, good mass-and-size parameters and the possibility of an arbitrary configuration of transport lines. At the same time such a drawback of LHPs of the conventional type as the instability of start up and operation in the region of low heat loads reduces their performance. The problem is connected, in a general case, with the unfavourable distribution of the vapor and the liquid phases of the working fluid in the evaporator. There is reason to believe that the LHP operation can also be significantly affected by zero-g conditions, in which the distribution of a working fluid is pre-determined only by the action of surface forces and the thermocapillary phenomena. The paper performs a general analysis of the necessary conditions imposed on the construction of LHP and some designs that contribute to the retention of serviceability in zero-g conditions at low heat loads. It gives the results of laboratory investigations of an adapted ammonia LHP with a heat-transfer capacity up to 2 kWxm
Найти похожие

13.

Вид документа :
Шифр издания : 53/M 73
Автор(ы) : Pastukhov V. G., Maydanik Yu. F., Vershinin S. V., Korukov M. A.
Заглавие : Miniature loop heat pipes for electronics cooling
Место публикации : Applied Thermal Engineering : 12th International Heat Pipe Conference Location, Russia, 19-24 may 2002 . - 2003. - Vol.23, № 9. - С. 1125-1135
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): miniature loop heat pipe--cpu--thermal resistance
Аннотация: The paper is devoted to the development of miniature loop heat pipes (mLHPs) with a nominal capacity of 25-30 W and a heat-transfer distance up to 250 mm intended for cooling electronics components and CPU of mobile PC. It gives the results of investigating several prototypes of mLHPs incorporated into remote heat exchanger (RHE) systems in different conditions. It has been established that in the nominal range of heat loads orientation does not practically affect the mLHPs operating characteristics. Under air cooling the total thermal resistance of such a system is 1.7-4.0degreesC/W and depends strongly on the cooling conditions and the radiator efficiency. In this case the mLHP's own thermal resistance is in the limits from 0.3 to 1.2degreesC/W, and the maximum capacity reaches 80-120 BT. The obtained results make it possible to regard mLHPs as quite promising devices for RHE systems providing thermal regimes for electronics components and personal computers. (C) 2003 Elsevier Science Ltd. All rights reserved
Найти похожие

14.

Вид документа :
Шифр издания : 53/M 73
Автор(ы) : Pastukhov V. G., Maydanik Yu. F., Vershinin S. V., Korukov M. A.
Заглавие : Miniature loop heat pipes for electronics cooling
Место публикации : Applied Thermal Engineering : 12th International Heat Pipe Conference Location, Russia, 19-24 may 2002 . - 2003. - Vol.23, № 9. - С. 1125-1135
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): miniature loop heat pipe--cpu--thermal resistance
Аннотация: The paper is devoted to the development of miniature loop heat pipes (mLHPs) with a nominal capacity of 25-30 W and a heat-transfer distance up to 250 mm intended for cooling electronics components and CPU of mobile PC. It gives the results of investigating several prototypes of mLHPs incorporated into remote heat exchanger (RHE) systems in different conditions. It has been established that in the nominal range of heat loads orientation does not practically affect the mLHPs operating characteristics. Under air cooling the total thermal resistance of such a system is 1.7-4.0degreesC/W and depends strongly on the cooling conditions and the radiator efficiency. In this case the mLHP's own thermal resistance is in the limits from 0.3 to 1.2degreesC/W, and the maximum capacity reaches 80-120 BT. The obtained results make it possible to regard mLHPs as quite promising devices for RHE systems providing thermal regimes for electronics components and personal computers. (C) 2003 Elsevier Science Ltd. All rights reserved
Найти похожие

15.

Вид документа : Статья из журнала
Шифр издания : 53/M 19
Автор(ы) : Maydanik Yu. F., Fershtater Y. G., Goncharov K.
Заглавие : Capillary-pump loop for systems of thermal regulation of spacecraft
Место публикации : Proceedings 4th European Symposium on Space Environmental Control Systems (Florence, Italy, 1991). - Florence, 1991. - С. 87-92
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): контур капиллярной прокачки--система термического регулирования--аппарат космический--космический аппарат
Найти похожие

16.

Вид документа : Статья из журнала
Шифр издания : 53/M 19
Автор(ы) : Maydanik Yu. F., Fershtater Y. G., Goncharov K.
Заглавие : Capillary-pump loop for systems of thermal regulation of spacecraft
Место публикации : Proceedings 4th European Symposium on Space Environmental Control Systems (Florence, Italy, 1991). - Florence, 1991. - С. 87-92
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): контур капиллярной прокачки--система термического регулирования--аппарат космический--космический аппарат
Найти похожие

17.

Вид документа : Статья из журнала
Шифр издания : 53/I-60
Автор(ы) : Zhelezny V. P., Zhelezny P. V., Skripov P.V., Vozniy V. F., Procenko D. A., Ancherbak S. N.
Заглавие : Influence of admixtures of the compressor oil to the enthalpy of working fluid in evaporator
Место публикации : Compressors 2004, International Conference on Compressors and Coolants, 5th, Casta Papiernicka, Slovakia, Sept. 29-Oct. 1, 2004. - 2004. - С. 303-309
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): admixtures
Найти похожие

18.

Вид документа : Статья из журнала
Шифр издания : 53/I-60
Автор(ы) : Zhelezny V. P., Zhelezny P. V., Skripov P.V., Vozniy V. F., Procenko D. A., Ancherbak S. N.
Заглавие : Influence of admixtures of the compressor oil to the enthalpy of working fluid in evaporator
Место публикации : Compressors 2004, International Conference on Compressors and Coolants, 5th, Casta Papiernicka, Slovakia, Sept. 29-Oct. 1, 2004. - 2004. - С. 303-309
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): admixtures
Найти похожие

19.

Вид документа :
Шифр издания : 53/H 65
Автор(ы) : North M. T., Sarraf D. B., Rosenfeld J. H., Maydanik Yu. F., Vershinin S. V.
Заглавие : High heat flux loop heat pipes
Место публикации : SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM (STAIF-97), PTS 1-3: 1ST CONFERENCE ON FUTURE SCIENCE & EARTH SCIENCE MISSIONS; 1ST CONFERENCE ON SYNERGISTIC POWER & PROPULSION SYSTEMS TECHNOLOGY; 1ST CONFERENCE ON APPLICATIONS OF THERMOPHYSICS IN MICROGRAVITY; 2ND CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; - 2ND CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 14TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION, ALBUQUERQUE, 26-30 JAN, 1997 . - 1997. - Vol.387. - С. 561-566
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --thermal power loads--vapor flow losses
Аннотация: Loop Heat Pipes (LHPs) can transport very large thermal power loads, over long distances, through flexible, small diameter tubes and against high gravitational heads. While recent LHPs have transported as much as 1500 W, the peak heat flux through a LHP's evaporator has been limited to about 0.07 MW/m(2). This limitation is due to the arrangement of vapor passages next to the heat load which is one of the conditions necessary to ensure self priming of the device. This paper describes work aimed at raising this limit by threefold to tenfold. Two approaches were pursued. One optimized the vapor passage geometry for the high heat flux conditions. The geometry improved the heat flow into the wick and working fluid. This approach also employed a finer pored wick to support higher vapor flow losses. The second approach used a bidisperse wick material within the circumferential vapor passages. The bidisperse material increased the thermal conductivity and the evaporative surface area in the region of highest heat flux, while providing a flow path for the vapor. Proof-of-concept devices were fabricated and tested for each approach. Both devices operated as designed and both demonstrated operation at a heat flux of 0.70 MW/m(2). This performance exceeded the known state of the art by a factor of more than six for both conventional heat pipes and for loop heat pipes using ammonia. In addition, the bidisperse-wick device demonstrated boiling heat transfer coefficients up to 100,000 W/m(2) K, and the fine pored device demonstrated an orientation independence with its performance essentially unaffected by whether its evaporator was positioned above, below or level with the condenser
Найти похожие

20.

Вид документа :
Шифр издания : 53/H 65
Автор(ы) : North M. T., Sarraf D. B., Rosenfeld J. H., Maydanik Yu. F., Vershinin S. V.
Заглавие : High heat flux loop heat pipes
Место публикации : SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM (STAIF-97), PTS 1-3: 1ST CONFERENCE ON FUTURE SCIENCE & EARTH SCIENCE MISSIONS; 1ST CONFERENCE ON SYNERGISTIC POWER & PROPULSION SYSTEMS TECHNOLOGY; 1ST CONFERENCE ON APPLICATIONS OF THERMOPHYSICS IN MICROGRAVITY; 2ND CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; - 2ND CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 14TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION, ALBUQUERQUE, 26-30 JAN, 1997 . - 1997. - Vol.387. - С. 561-566
ББК : 53
Предметные рубрики: ФИЗИКА
Ключевые слова (''Своб.индексиров.''): loop heat pipes --thermal power loads--vapor flow losses
Аннотация: Loop Heat Pipes (LHPs) can transport very large thermal power loads, over long distances, through flexible, small diameter tubes and against high gravitational heads. While recent LHPs have transported as much as 1500 W, the peak heat flux through a LHP's evaporator has been limited to about 0.07 MW/m(2). This limitation is due to the arrangement of vapor passages next to the heat load which is one of the conditions necessary to ensure self priming of the device. This paper describes work aimed at raising this limit by threefold to tenfold. Two approaches were pursued. One optimized the vapor passage geometry for the high heat flux conditions. The geometry improved the heat flow into the wick and working fluid. This approach also employed a finer pored wick to support higher vapor flow losses. The second approach used a bidisperse wick material within the circumferential vapor passages. The bidisperse material increased the thermal conductivity and the evaporative surface area in the region of highest heat flux, while providing a flow path for the vapor. Proof-of-concept devices were fabricated and tested for each approach. Both devices operated as designed and both demonstrated operation at a heat flux of 0.70 MW/m(2). This performance exceeded the known state of the art by a factor of more than six for both conventional heat pipes and for loop heat pipes using ammonia. In addition, the bidisperse-wick device demonstrated boiling heat transfer coefficients up to 100,000 W/m(2) K, and the fine pored device demonstrated an orientation independence with its performance essentially unaffected by whether its evaporator was positioned above, below or level with the condenser
Найти похожие

 1-20    21-36 
 

Сиглы отделов ЦНБ УрО РАН


  бр.ф. - Бронированный фонд

  бф - Научно-библиографический отдел

  БХЛ - Фонд художественной литературы

  ИИиА -Фонд исторической литературы в ЦНБ УрО РАН

  ИМЕТ -Отдел ЦНБ в Институте металлургии УрО РАН

  кх - Отдел фондов (книгохранениe)

  МБА - Межбиблиотечный абонемент

  мф - Методический фонд

  ок - Отдел научной каталогизации

  оку - Отдел комплектования и учета

  орф - Обменно-резервный фонд

  пф - Читальный зал деловой и патентной информации

  рк - Фонд редкой книги

  ч/з - Главный читальный зал

  эр - Зал электронных ресурсов

  

Сиглы библиотек институтов и НЦ УрО РАН
© Международная Ассоциация пользователей и разработчиков электронных библиотек и новых информационных технологий
(Ассоциация ЭБНИТ)
Яндекс.Метрика