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Landing performance of an air cushion landing system installed on a 1/10-scale dynamic model on the C-8 Buffalo airplaneAn experimental study was conducted to evaluate the landing behavior of a 1/10-scale dynamic model of the C-8 Buffalo airplane equipped with an air-cushion landing system (ACLS) on a variety of surfaces including both calm and rough water and a smooth hard surface. Taxi runs were made on the hard surface over several obstacles. Landings were made with the model at various pitch and roll attitudes and vertical velocities and at one nominal horizontal velocity. Data from the landings include time histories of the trunk and air-cushion pressures and accelerations at selected locations on the model.
Document ID
19730021300
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Thompson, W. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-7295
L-8724
Report Number: NASA-TN-D-7295
Report Number: L-8724
Accession Number
73N30032
Funding Number(s)
PROJECT: RTOP 501-38-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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