Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /
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Author / Creator: | Noonan, Kevin W., author. |
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Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. |
Description: | 1 online resource (82 pages) : chiefly illustrations. |
Language: | English |
Series: | NASA technical paper ; 1701 AVRADCOM technical report ; 80-B-5 NASA technical paper ; 1701. AVRADCOM technical report ; 80-B-5. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10914300 |
Other authors / contributors: | Bingham, Gene J., author. Langley Research Center. United States. Army Aviation Research and Development Command. Army Research and Technology Laboratories (U.S.). Structures Laboratory. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. |
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Notes: | Title from title screen (viewed on Aug. 16, 2016). "September 1980." "Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page. Includes bibliographical references (page 13). Technical paper. National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02 L-13139 |
Other form: | Print version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 Microfiche version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 |
GPO item no.: | 0830-H-15 (online) |
Govt.docs classification: | NAS 1.60:1701 |
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