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Pressure distribution data from tests of 2.29 M (7.5 feet) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnelA high-lift transport aircraft model equipped with full-span leading-edge slat and part-span double-slotted trailing-edge flap was tested in the Ames 12-ft pressure tunnel to determine the low-speed performance characteristics of a representative high-aspect-ratio supercritical wing. These tests were performed in support of the Energy Efficient Transport (EET) program which is one element of the Aircraft Energy Efficiency (ACEE) project. Static longitudinal forces and moments and chordwise pressure distributions at three spanwise stations were measured for cruise, climb, two take-off flap, and two landing flap wing configurations. The tabulated and plotted pressure distribution data is presented without analysis or discussion.
Document ID
19850021600
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kjelgaard, S. O. (NASA Langley Research Center Hampton, VA, United States)
Morgan, H. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1983
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:84517
NASA-TM-84517
Accession Number
85N29912
Funding Number(s)
PROJECT: RTOP 505-45-43-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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