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SAE AIR4065A

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Soveltamisala

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 , η 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.

Julkaisun tiedot

  • Standardi julkaisijalta SAE International
  • Julkaistu:
  • Julkaisutyyppi: IS
  • Julkaisija SAE International
  • Jakelija SAE International

Sidokset

  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE ARP921
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AIR1703
  • Korvaa: SAE AIR4065
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AS8006
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AIR1678
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE ARP755
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE ARP1217
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AS8009
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AS8005
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE ARP920