SAE AIR1706C
Current
The latest, up-to-date edition.
The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing
Hardcopy , PDF
English
08-01-2010
1 SCOPE
1.1 Purpose
2 REFERENCES
3 GENERAL FEATURES OF AECS
4 AECS COMPUTER PROGRAM
4.1 History of Program
4.2 AECS Capabilities
4.3 Program Organization
4.4 General Methods of Solution
4.5 Modes of Operation
4.5.1 Performance Mode
4.5.2 Sizing Mode
4.6 Model Definition
4.6.1 Problem Description
4.6.2 Use of Component Identifier Subroutines
4.6.3 Data Preparation
4.7 Problem Input
4.7.1 Performance Input
4.7.2 Sizing Input
4.8 Control Options
4.9 Program Output
4.9.1 Performance Output
4.9.2 Sizing Output
4.10 Computer System
5 USAGE
5.1 Types of Application
5.2 Program Capabilities and Limitations
5.2.1 Capabilities
5.2.2 Limitations
5.3 Improvements Needed
Specifies capabilities, limitations, and potentials of a particular computer program which provides a general ECS analysis capability, and is available for use in industry.
DocumentType |
Standard
|
Pages |
20
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This document has been declared “CANCELLED” as of January 2010. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index.
SAE AIR 1277 : 2005 | COOLING OF MILITARY AVIONIC EQUIPMENT |
SAE ARP 217 D : 2016 | TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS) |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.