NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
9- by 15-Foot Low-Speed Wind Tunnel Commissioning Test Using Advanced Ducted PropulsorA subscale model of an aircraft engine fan was tested in the 9- by 15-Foot Low-Speed Wind Tunnel at the NASA Glenn Research Center in 2022. The fan model was the Advanced Ducted Propulsor Fan 1 designed by Pratt & Whitney in the 1990s. It has been part of multiple wind tunnel test campaigns over the last 30 years. The 2022 test served two purposes: to commission the wind tunnel for fan and propulsor testing after a test facility improvement project and to generate a new data set with the latest data systems and processing improvements. This report documents the test and provides highlights of the aerodynamic and acoustic data that was generated. A supplemental data package that includes several parts (TM-20250004035-SUPPL.zip) accompanies this report.
Document ID
20250004035
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
David B Stephens
(Glenn Research Center Cleveland, United States)
David M Elliott
(Glenn Research Center Cleveland, United States)
John A Gazzaniga
(HX5 (United States) Fort Walton Beach, Florida, United States)
Date Acquired
April 22, 2025
Publication Date
July 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Acoustics
Aerodynamics
Report/Patent Number
NASA/TM-20250004035
E-20324
Funding Number(s)
WBS: 081876.02.03.19.01.01.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
turbofan
wind tunnel
aeronautics
propulsion
acoustics
No Preview Available