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Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type AirplaneThe lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering flight over the Mach number range from 0.70 to 0.85 for the airplane in the clean configuration at an altitude of 26,000 feet. Data were also obtained over the speed range of 130 knots to 160 knots at 9,000 feet for various flap deflections with gear down.
Document ID
19980227097
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Tambor, Ronald (NASA Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1960
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TN-D-30
H-119
Report Number: NASA-TN-D-30
Report Number: H-119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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