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Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic SpeedsThe data contained on this CD are a supplement to NASA/TP-2001-210629 published in February 2001. This CD replaces a web-site database search and retrieval system - noted as reference 36 in the NASA/TP - that was to supply the aeronautical community with access to the flight data. Unfortunately, this web-site was only available for a short time after the publication of NASA/TP-2001-21068 due to software and support issues. The contents of this CD are organized into five folders containing data from the flight test and reference 1. In particular, the following are provided: (1) tabular data of the Flight Conditions from Table 5; (2) boundary layer data from Table 12 for three flights in multiple formats; (3) skin-friction data - xmgr format (ref. 3) - used to generate Figure 26; (4) surface pressure data with a listing of the parameters; and (5) tuft-images from three cameras in two formats.
Document ID
20090004590
Acquisition Source
Langley Research Center
Document Type
Other - Flight Test Data Zipfile ( Supplement to NASA/TP-2001-210629)
Authors
John E Lamar
(Langley Research Center Hampton, Virginia, United States)
Clifford J Obara
(Langley Research Center Hampton, Virginia, United States)
Bruce D Fisher
(Langley Research Center Hampton, Virginia, United States)
David F Fisher
(Armstrong Flight Research Center Rosamond, California, United States)
Date Acquired
August 24, 2013
Publication Date
June 10, 2008
Subject Category
Aerodynamics
Report/Patent Number
NASA/TP-2001-210629/SUPPL
L-19482
Funding Number(s)
WBS: 526282.01.07.04.01
WORK_UNIT: 522-31-31-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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