Aircraft fuel tank entry wall-projectile interaction studies.

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Authors
Bates, Kenneth Scott
Subjects
Advisors
Power, H.L.
Date of Issue
1973-06
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Hydraulic ram is the physical production of pressure wave wall loadings due to projectile penetration and their effect on a fuel cell. Facilities were designed and testing conducted in preparation for investigation of the hydraulic ram phenomenon. A ballistic range was designed that yielded projectile velocity and flight attitude information before and after wall penetration. Wall specimens of a single thickness were impacted by a range of projectile sizes, weights, shapes, and velocities. This yielded the energy absorbed by the wall without fluid damping.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School
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NPS Report Number
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Citation
Distribution Statement
Approved for public release; distribution is unlimited.
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