Show simple item record

contributor authorG. D. Huffman
contributor authorO. E. Buxton
date accessioned2017-05-09T00:06:41Z
date available2017-05-09T00:06:41Z
date copyrightJanuary, 1968
date issued1968
identifier issn1528-8919
identifier otherJETPEZ-26667#89_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126312
description abstractThe design of a space power system yielding maximum performance is a laborious task requiring implicit knowledge of many criteria. The labor involved with previous techniques is not conducive to the analysis of systems employing novel fluids. To circumvent these problems, a new method of analysis of saturated and superheated Rankine cycles is presented. The approach employed equates maximum performance with the minimum radiating area which can then be linked to a particular cycle through thermodynamic relationships. The analysis is concluded by utilizing a semiempirical technique to determine turbine efficiencies. The new approach which is applicable to all fluids is then used to evaluate three typical cycles.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermodynamic Optimization of Rankine Cycle Space Power Systems
typeJournal Paper
journal volume90
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3609139
journal fristpage89
journal lastpage96
identifier eissn0742-4795
keywordsPower systems (Machinery)
keywordsOptimization
keywordsRankine cycle
keywordsCycles
keywordsFluids
keywordsSuperheating
keywordsTurbines
keywordsSystems analysis AND Design
treeJournal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record