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
Resource Information
The work 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 represents a distinct intellectual or artistic creation found in Indiana State Library. This resource is a combination of several types including: Work, Language Material, Books.
The Resource
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
Resource Information
The work 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 represents a distinct intellectual or artistic creation found in Indiana State Library. This resource is a combination of several types including: Work, Language Material, Books.
- Label
- 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
- Title number
- Volume 1
- Title part
- Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec
- Statement of responsibility
- Joe W. Elliott ... [and others]
- Language
- eng
- Cataloging source
- GPO
- Government publication
- federal national government publication
- Index
- no index present
- Literary form
- non fiction
- Series statement
-
- AVSCOM TR
- NASA technical memorandum
- Series volume
-
- 92-B-003
- 104224
Context
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/sDRUOh87zdc/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/sDRUOh87zdc/">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</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/sDRUOh87zdc/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/sDRUOh87zdc/">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</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
