SAE AIR4065A

SAE AIR4065A – Propeller/Propfan In-Flight Thrust Determination (Stabilized: May 2012)

This document has been declared “Stabilized” and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

AIR 4065 “Propeller/Propfan In-Flight Thrust Determination” addresses steady state propeller thrust as applied to aircraft which are usually powered by gas turbine engines. It includes theory examples and methods which have been used. Specifically two methods are discussed the “J” or traditional J Cdp Cdt gn method including the SBAC variation and a new method we call the “Theta” method which is dependent on knowing blade angle power/torque and flight Mach number. Implementation guidelines are offered as well as overall approaches to flight testing. Appendices include expansions on theory and testing as well as examples.

Product Details

Published:

05/29/2012

File Size:

1 file 11 MB

Note:

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