GLTRS--Glenn
TITLE AND SUBTITLE:
Wind Tunnel Measured Effects on a Twin-Engine Short-Haul Transport Caused by Simulated Ice Accretions Data Report

AUTHOR(S):
Andrew Reehorst, Mark Potapczuk, Thomas Ratvasky, and Brenda Gile Laflin

REPORT DATE:
May 1997

FUNDING NUMBERS:
WU-548-20-23

PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES):
National Aeronautics and Space Administration
Lewis Research Center
Cleveland, Ohio 44135-3191

PERFORMING ORGANIZATION REPORT NUMBER:
E-10659

SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES):
National Aeronautics and Space Administration
Washington, DC 20546-0001

REPORT TYPE AND DATES COVERED:
Technical Memorandum

SPONSORING/MONITORING AGENCY REPORT NUMBER:
NASA TM-107419

SUPPLEMENTARY NOTES:
Data report for TM107143, which bears the same title. Andrew Reehorst, Mark Potapczuk, and Thomas Ratvasky, NASA Lewis Research Center; Brenda Gile Laflin, NASA Langley Research Center, Hampton, Virginia, 23681-0001. Responsible person, Andrew Reehorst, organization code 5840, (216) 433-3938.

ABSTRACT:
The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tunnel test that examined icing effects on a 1/8 scale twin-engine short-haul jet transport model. Presented in this document are summary data from the major configurations tested. The entire test database in addition to ice shape and model measurements is available as a data supplement in CD-ROM form. Data measured and presented are: wing pressure distributions, model force and moment, and wing surface flow visualization.

SUBJECT TERMS:
Aircraft icing; Wind tunnel; Aircraft performance; Flow visualization

NUMBER OF PAGES:
102

PDF AVAILABLE FROM URL:
1997/TM-107419.pdf
(8,067,561 KB)
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