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Revision A, November 1, 1986

Complete Document

Cooling Data for Turbine Engines in Helicopters

Includes all amendments and changes through Reaffirmation Notice , May 1991

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Active, Most Current

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Product Details:

  • Revision: Revision A, November 1, 1986
  • Published Date: May 1991
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 29
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Method: A tested method of data presentation and use is described herein. The method shown is a useful guide, to he used with care and to be improved with use.

Axial Nacelle Air Flow: Machine computer programs and an example problem are given for axial nacelle air flow.

Transverse Nacelle Air Flow: Calculation is given for natural and forced convection with example problems.
AIA/NAS Aerospace Standards