• SAE AIR5687A

SAE AIR5687A

  • Inlet/Engine Compatibility - From Model to Full Scale Development (Stabilized: Feb 2016)
  • standard by SAE International, 02/16/2016
  • Category: SAE

$81.00 $41.00

This document reviews the state of the art for data scaling issues associated with air induction system development for turbine-engine-powered aircraft. In particular, the document addresses issues with obtaining high quality aerodynamic data when testing inlets. These data are used in performance and inlet-engine compatibility analyses. Examples of such data are: inlet recovery, inlet turbulence, and steady-state and dynamic total-pressure inlet distortion indices. Achieving full-scale inlet/engine compatibility requires a deep understanding of three areas: 1) geometric scaling fidelity (referred to here as just “scaling”), 2) impact of Reynolds number, and 3) ground and flight-test techniques (including relevant environment simulation, data acquisition, and data reduction practices). The Model-to-Full Scale Subcommittee of the S-16 Turbine Engine Inlet Flow Distortion Committee has examined archives and has obtained recollections of experts regarding air induction system development experience to produce this document.

PDF

All of our standards document are available in PDF (Portable Document Format), an electronic, downloadable format.You will be able to download the file in your account downloads.

Multi-User Access

After purchasing, you have the ability to assign each license to a specific user.

Printable

At any time, you are permitted to make printed copies for your and your members' reference use.

SAE AS8017D

SAE AS8017D

Minimum Performance Standard for Anticollision Light Systems..

$41.00 $81.00

SAE ARP4168B

SAE ARP4168B

Night Vision Goggle (NVG) Compatible Light Sources..

$41.00 $81.00

SAE AMS4893D

SAE AMS4893D

Alloy Castings, Corrosion and Heat-Resistant 66Ni - 29Cu - 4.0Si Solution Treated..

$41.00 $81.00

SAE J645_201708

SAE J645_201708

Automotive Transmission Terminology..

$41.00 $81.00