Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight. Volume 1, Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec [microform] / Joe W. Elliott [and others]
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| Corporate Authors: | , |
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| Other Authors: | |
| Format: | Government Document Microfilm Book |
| Language: | English |
| Published: |
Hampton, Va. : [St. Louis, Mo.] :
National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R&T Activity,
[1992]
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| Series: | AVSCOM technical report ;
92-B-3. NASA technical memorandum ; 104224. |
| Subjects: |
Norlin Library - Government Information - Microform
| Call Number: |
NAS 1.15:104224
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| NAS 1.15:104224 | Restricted Place a Hold |