A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.
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| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2014
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| Online Access: | http://hdl.handle.net/1721.1/86252 |
| _version_ | 1826204582029557760 |
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| author | Shaw, John, Jr |
| author2 | Rene H. Miller. |
| author_facet | Rene H. Miller. Shaw, John, Jr |
| author_sort | Shaw, John, Jr |
| collection | MIT |
| description | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S. |
| first_indexed | 2024-09-23T12:57:44Z |
| format | Thesis |
| id | mit-1721.1/86252 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T12:57:44Z |
| publishDate | 2014 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/862522019-04-10T09:03:40Z A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. Shaw, John, Jr Rene H. Miller. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Aeronautics and Astronautics Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S. Microfiche copy available in Barker. Bibliography: leaves 95-96. M.S. 2014-04-25T15:46:45Z 2014-04-25T15:46:45Z 1967 Thesis http://hdl.handle.net/1721.1/86252 24013424 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 ix, 96 leaves application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics Shaw, John, Jr A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title | A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title_full | A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title_fullStr | A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title_full_unstemmed | A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title_short | A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control. |
| title_sort | feasibility study of helicopter vibration reduction by self optimizing higher harmonic blade pitch control |
| topic | Aeronautics and Astronautics |
| url | http://hdl.handle.net/1721.1/86252 |
| work_keys_str_mv | AT shawjohnjr afeasibilitystudyofhelicoptervibrationreductionbyselfoptimizinghigherharmonicbladepitchcontrol AT shawjohnjr feasibilitystudyofhelicoptervibrationreductionbyselfoptimizinghigherharmonicbladepitchcontrol |