| Title: | Derivation of a tapered p-version beam finite element |
| Author: | Hinnant, Howard E. |
| Author: | Langley Research Center. Aerostructures Directorate |
| Note: | National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989 |
| Link: | page images at HathiTrust |
| No stable link: | This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links. |
| Subject: | Airframes -- Vibration -- Mathematical models |
| Subject: | Finite element method |
| Subject: | Girders -- Vibration -- Mathematical models |
| Subject: | Helicopters -- Vibration -- Mathematical models |
| Subject: | Structural analysis (Engineering) |
| Subject: | Vibration (Aeronautics) -- Mathematical models |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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