NDLI: 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 tunnel

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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 tunnel

Content Provider	NASA Technical Reports Server (NTRS)
Author	Morgan Jr., H. L. Kjelgaard, S. O.
Copyright Year	1983
Description	A 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.
File Size	21736220
Page Count	676
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19850021600
Archival Resource Key	ark:/13960/t6g20tk3g
Language	English
Publisher Date	1983-04-01
Access Restriction	Open
Subject Keyword	Aeronautics (general) Aircraft Models Tables Data High Aspect Ratio Transport Aircraft Efficiency Leading Edge Slats Pressure Distribution Supercritical Wings Trailing Edge Flaps Graphs Charts Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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