SAE AIR 1823 : 1996

Withdrawn

ENGINEERING ANALYSIS SYSTEM (EASY) COMPUTER PROGRAM FOR DYNAMIC ANALYSIS OF AIRCRAFT ECS

Available format(s)

Hardcopy , PDF

Withdrawn date

25-05-2011

Language(s)

English

Published date

01-01-1996

Publisher

SAE International

1 SCOPE
  1.1 Purpose
2 REFERENCES
  2.1 SAE Publications
  2.2 Other References
  2.3 Definitions
3 BACKGROUND ON COMPUTERIZED TRANSIENT ECS ANALYSIS
4 GENERAL FEATURES OF EASY
  4.1 Analysis Capabilities
  4.2 Usage Aspects
5 EASY COMPUTER PROGRAM
  5.1 History of Program
  5.2 EASY Program Capabilities
  5.3 Program Organization
      5.3.1 Model Generation Program
      5.3.2 Analysis Program
      5.3.3 File Maintenance Program
  5.4 Problem Input
      5.4.1 Model Generation Program Input
      5.4.2 Analysis Program Input
  5.5 Program Output
      5.5.1 Model Generation Program Output
      5.5.2 Analysis Program Output
  5.6 Computer System
6 LIMITATIONS AND OTHER USAGE
  6.1 Limitations
  6.2 Usage on Other Types of Systems
  6.3 EASY4, EASY5(CE), EASY5, and EASY5x
APPENDIX A - SAMPLE EASY INPUT AND OUTPUT
FIGURES
TABLES

Specifies techniques for analysis of steady-state and dynamic (transient) environmental control system (ECS) performance, control system stability, and for synthesis of optimal ECS.

Committee	AC-9
DocumentType	Standard
Pages	31
PublisherName	SAE International
Status	Withdrawn

SAE ARP 217 D : 2016	TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
SAE AIR 1277 : 2005	COOLING OF MILITARY AVIONIC EQUIPMENT
SAE ARP 89 : 2012	AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM