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Flight Tests of an Airplane Model with 42 Degree Swept-back Wing in the Langley Free-flight Tunnel
Document ID
19930081903
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Maggin, Bernard
Bennett, Charles V
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1287
Report Number: NACA-TN-1287
Accession Number
93R11193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, SWEPTBACK - STABILITY, LONGITUDINAL
INTERFERENCE - TAIL SURFACES & WINGS
AIRFOILS - NACA 0009 TAIL SURFACE
WIND TUNNEL TESTS - NACA - FREE-FLIGHT WORK CARRIED ON AT LMAL
STABILITY
STABILITY & CONTROL
STALLING - SWEPTBACK WINGS
TAIL SURFACES - POSITION

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