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Flight Investigation of the Effects of Horizontal-tail Height, Moment of Inertia, and Control Effectiveness on the Pitch-up Characteristics of a 35 Degree Swept-wing Fighter Airplane at High Subsonic Speeds
Document ID
19930088281
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mcfadden, Norman M
Heinle, Donovan R
Date Acquired
August 16, 2013
Publication Date
January 18, 1954
Report/Patent Number
NACA-RM-A54F21
Report Number: NACA-RM-A54F21
Accession Number
93R17571
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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