DI-TMSS-81515B

User’s Manual for Gas Turbine Engine Steady‐State and Transient Performance Presentation for Digital Computer Programs

contributor author	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned	2017-09-04T17:41:23Z
date available	2017-09-04T17:41:23Z
date copyright	07/10/2012
date issued	2012
identifier other	DXVKXEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho1513AF679D40AC4261598F1EFDEC014A/handle/yse/164411
description abstract	Use/relationship: This Data Item Description (DID) provides the method for presentation of gas turbine engine steady‐state and transient performance calculated using digital computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight and dimensions computed by digital computer programs. The information is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. a. This DID contains the format, content and intended use of information for the data resulting from the work task described in the Society of Automotive Engineers (SAE) Aerospace Standard 681 and SAE Aerospace Standard 755. b. DI‐TMSS‐81515B supersedes DI‐TMSS‐81515A.
language	English
title	DI-TMSS-81515B	num
title	User’s Manual for Gas Turbine Engine Steady‐State and Transient Performance Presentation for Digital Computer Programs	en
type	standard
page	1
status	Active
tree	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;2012
contenttype	fulltext