AIR4065 Propeller/Propfan In-Flight Thrust Determination

Reaffirmed

11/17/2004

Scope
Content
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,C p ,C t ,ν 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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR4065
Pages
215
Citation
SAE International Information Report, Propeller/Propfan In-Flight Thrust Determination, SAE Standard AIR4065, Reaffirmed November 2004, https://doi.org/10.4271/AIR4065.
Additional Details
Publisher
Published
Nov 17, 2004
Product Code
AIR4065
Content Type
Information Report
Status
Reaffirmed
Language
English

Revisions