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ISO 1133-1997 塑料热塑性塑料熔体质量流动速率(MFR)和熔体体积流动速率(MVR)的测定

上一篇: ISO 10931-1-1997 工业用塑料管道系统聚偏氟乙烯(PVDF)第1部分:总则
下一篇: ISO 4250-2 AMD 1-1997 土方机械轮胎和轮辋第2部分:载重和充气压力修改1

【英文标准名称】:PracticeforCalculatingtheContrastandThresholdSensitivityofaPositivePhotoresist
【原文标准名称】:计算正性光致抗蚀剂的对比度和阈限灵敏度
【标准号】:ASTMF1059-1987(1992)
【标准状态】:作废
【国别】:
【发布日期】:1987
【实施或试行日期】:
【发布单位】:美国材料与试验协会(US-ASTM)
【起草单位】:
【标准类型】:(Practice)
【标准水平】:()
【中文主题词】:数学计算;工艺;电子工程;灵敏度;光导电池;感光度
【英文主题词】:
【摘要】:
【中国标准分类号】:G84
【国际标准分类号】:
【页数】:
【正文语种】:


Product Code:SAE AIR1703
Title:In-Flight Thrust Determination
Issuing Committee:E-33 In Flight Propulsion Measurement Committee
Scope: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.
Rationale: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.

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