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High lift aerodynamicsThe current program is aimed at providing a physical picture of the flow physics and quantitative turbulence data of the interaction of a high Reynolds number wake with a flap element. The impact of high lift on aircraft performance is studied for a 150 passenger transport aircraft with the goal of designing optimum high lift systems with minimum complexity.
Document ID
19940020786
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sullivan, John (Purdue Univ. West Lafayette, IN, United States)
Schneider, Steve (Purdue Univ. West Lafayette, IN, United States)
Campbell, Bryan (Purdue Univ. West Lafayette, IN, United States)
Bucci, Greg (Purdue Univ. West Lafayette, IN, United States)
Boone, Rod (Shaw Univ. Raleigh, NC., United States)
Torgerson, Shad (Purdue Univ. West Lafayette, IN, United States)
Erausquin, Rick (Purdue Univ. West Lafayette, IN, United States)
Knauer, Chad (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 6, 2013
Publication Date
March 8, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-195183
NAS 1.26:195183
Report Number: NASA-CR-195183
Report Number: NAS 1.26:195183
Accession Number
94N25268
Funding Number(s)
CONTRACT_GRANT: NAG2-854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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