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Results of Measurements of Maximum Lift and Buffeting Intensities Obtained During Flight Investigation of the Northrop X-4 Research AirplaneThe variation of the intensity of buffeting experienced throughout the operational region of the semitailless Northrop X-4 airplane and the values of maximum and peak normal-force coefficients in the Mach number range from 0.42 to 0.92 have been determined. The results are compared with data obtained with the swept-wing Douglas D-558-II airplane.
Document ID
19930087804
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Baker, Thomas F
Date Acquired
August 16, 2013
Publication Date
August 20, 1953
Report/Patent Number
NACA-RM-L53G06
Report Number: NACA-RM-L53G06
Accession Number
93R17094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLYING QUALITIES
CONTROL, LONGITUDINAL
STALLING
MACH NUMBER EFFECTS - COMPLETE WINGS
VIBRATION AND FLUTTER - BODIES
AIRPLANES - SPECIFIC TYPES

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