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Influence of static longitudinal stability on the behavior of airplanes in gustsThe equations of motion for an airplane penetrating a gust are derived using a few simplifying assumptions. Calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, are compared with flight tests. Good agreement is obtained between the trend of the flight tests and the calculated values; however no absolute comparison was possible between the flight tests and calculations.
Document ID
19930093907
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoene, H
Date Acquired
August 16, 2013
Publication Date
November 1, 1951
Report/Patent Number
NACA-TM-1323
Report Number: NACA-TM-1323
Accession Number
93R23233
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOADS, GUST - HENSCHEL 122
EQUATIONS - MOTION
LOADS, GUST - HEINKEL 45
LOADS, GUST - WINGS
STABILITY, LONGITUDINAL - STATIC
LOADS, GUST

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