Structural design analysis of the Tail Landing Gear Bay and the vertical/horizontal stabilizers of the RAH-66 comanche helicopter
Approved for public release; distribution is unlimited === The RAH-66 Comanche's stealth design requires the use of radar- absorbing material (RAM) on the outer skin of the aircraft. The reduced stiffness properties of RAM produce insufficient tail torsional stiffness, necessitating the use of...
Main Author: | Shoop, Brian P |
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Other Authors: | Wood, E. Roberts |
Language: | English |
Published: |
Monterey, California. Naval Postgraduate School
2012
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Online Access: | http://hdl.handle.net/10945/9020 |
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