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F-16XL Interview with Marta Bohn-MeyerMarta Bohn-Meyer discusses the cooperative research between Rockwell Industries and NASA research facilities in their effort to optimize and maintain the supersonic laminar flow on the F-16XL aircraft. Research on the airfoil design, chord optimization, introduction of a suction feature to maintain pressure distribution, and CFD, both theoretical and actual phenomena, are discussed. Bohn-Meyer discusses the difference between supersonic and subsonic laminar flow, cross flow, reasons behind using this particular F-16 aircraft for this research, and the future of this ongoing research, including the data base that investigators are building from wind tunnel data and in-flight validation.
Document ID
19950013580
Acquisition Source
Legacy CDMS
Document Type
Video
Date Acquired
August 16, 2013
Publication Date
July 27, 1992
Subject Category
Aerodynamics
Report/Patent Number
NONP-NASA-VT-95-41117
NASA-TM-110505
Accession Number
95N19996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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