Flight Data Pertinent to Buffeting and Maximum Normal-force Coefficient of the Douglas X-3 Research Airplane
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Baker, Thomas F↗
Engineering topics
Baker, Thomas F
Publications and source records attributed to Baker, Thomas F.
A Study of the Correlation Between Flight and Wind-Tunnel Buffeting Loads
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Huston, Wilber B↗
Flight Measurements at Transonic Speeds of the Buffeting Characteristics of the XF-92A Delta-wing Research Airplane
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Baker, Thomas F↗
Measured Data Pertaining to Buffeting at Supersonic Speeds of the Douglas D-558-II Research Airplane
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Baker, Thomas F↗
Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range from 0.5 to 0.95
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Baker, Thomas F↗
Results of Measurements of Maximum Lift and Buffeting Intensities Obtained During Flight Investigation of the Northrop X-4 Research Airplane
The 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.
FLYING QUALITIES↗
Some Measurements of the Buffet Region of a Swept-wing Research Airplane During Flights to Supersonic Mach Numbers
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Baker, Thomas F↗