Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
Resource Information
The work Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads represents a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries. This resource is a combination of several types including: Work, Language Material, Books.
The Resource
Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
Resource Information
The work Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads represents a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries. This resource is a combination of several types including: Work, Language Material, Books.
- Label
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Statement of responsibility
- John T. Batina
- Language
- eng
- Additional physical form
- Also available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.
- Cataloging source
- GPO
- Government publication
- federal national government publication
- Index
- no index present
- Literary form
- non fiction
- Series statement
- NASA technical memorandum
- Series volume
- 86320
Context
Context of Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloadsWork of
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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.umsl.edu/resource/bPSu9ju_Rmc/" typeof="CreativeWork http://bibfra.me/vocab/lite/Work"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/bPSu9ju_Rmc/">Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
