The Effect of Installation Power Losses on the Overall Performance of a Helicopter
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Product Code: AIR5642
Date Published: 2005-06-07
Issuing Committee:
S-12 Helicopter Powerplant Committee
Scope
The purpose of this SAE Aerospace Information Report (AIR) is to illustrate the effect of installation power losses on the performance of a helicopter. Installation power losses result from a variety of sources, some associated directly with the basic engine installation, and some coming from the installation of specific items of aircraft mission specific equipment. Close attention must be paid to the accurate measurement of these losses so that the correct aircraft performance is calculated.
Product Status: In Stock
File Size:
203K
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| Current & Historical versions of this standard |
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| Standard |
Date published |
?Status |
| AIR5642 |
2005-06-07 |
Issued |
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