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NF T76-159-2003 结构胶粘剂.在冲击条件下高强度胶粘剂黏结耐动态劈裂性的测定.楔形物冲击法

上一篇: NF T73-424-2003 表面活性剂.测定离子表面活性剂的临界溶解温度(克拉夫特点)和溶解度
下一篇: NF T73-279-2003 表面活性剂.用高性能液相色谱法测定线性烷基苯中二烃基萘满的含量

MIL-S-19653B (SH), MILITARY SPECIFICATION SEALING COMPOUND (WOOD BEDDING), FORTIFIED (27 JUL 1984)., This specification covers a permanently plastic, waterproofing sealing compound for use between inner and outer planking of double planked hulls, and on other faying surfaces of wooden craft to prevent the passage or accumulation of water and to resist deterioration by decay fungi.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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