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SAE AIR 5642 : 2005

SAE AIR 5642 : 2005

THE EFFECT OF INSTALLATION POWER LOSSES ON THE OVERALL PERFORMANCE OF A HELICOPTER

SAE International

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Table of Contents

INTRODUCTION
1 SCOPE
2 REFERENCES
3 INSTALLATION POWER LOSS MECHANISMS AND THEIR EFFECT ON
  ENGINE PERFORMANCE
4 POWER LOSSES ASSOCIATED WITH VARIOUS TYPES OF EQUIPMENT
5 TYPICAL LEVELS OF INSTALLED POWER LOSS
6 EFFECT OF INSTALLATION POWER LOSS ON HELICOPTER
  PERFORMANCE
APPENDIX A DETAILS OF HELICOPTER PERFORMANCE MODELLING

Abstract

Illustrates the effect of installation power losses on the performance of a helicopter.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee S-12

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