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Understanding 9/11Computational investigation of the compressible dynamic stall characteristics of the Sikorsky SSC-A09 airfoil
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Computational investigation of the compressible dynamic stall characteristics of the Sikorsky SSC-A09 airfoil
- Publication date
- 1993-09-01 00:00:00
- Topics
- Dynamic Stall, Supercritical Airfoil, Navier-Stokes Solution, Shock-induced Boundary Layer Separation
- Publisher
- Monterey, California. Naval Postgraduate School
- Collection
- navalpostgraduateschoollibrary; fedlink
- Language
- English
Steady and unsteady two-dimensional flowfield analysis was conducted for a Sikorsky SSC-AO9 airfoil in compressible, high Reynolds number flows. Limited verification with experimental measurement was achieved. Computational methods included a steady, line
- Addeddate
- 2019-04-26 00:31:42
- Advisor
- Platzer, Max Franz
Ekaterinaris, J.A.
- Corporate
- Naval Postgraduate School (U.S.)
- Degree_discipline
- Aeronautical Engineering
- Degree_grantor
- Naval Postgraduate School
- Degree_level
- Masters
- Degree_name
- M.S. in Aeronautical Engineering
- Department
- Aeronautics and Astronautics
- Distributionstatement
- Approved for public release; distribution is unlimited.
- Dspace_note
- Note, the Item of Record as published can be found at https://hdl.handle.net/10945/39957.
- External-identifier
- urn:handle:10945/39957
- Foldoutcount
- 0
- Identifier
- computationalinv1094539957
- Identifier-ark
- ark:/13960/t5r85z10p
- Item_source
- dspace
- Ocr
- tesseract 4.1.1
- Ocr_converted
- abbyy-to-hocr 1.1.4
- Ocr_detected_lang
- en
- Ocr_detected_lang_conf
- 1.0000
- Ocr_detected_script
- Latin
- Ocr_detected_script_conf
- 0.9449
- Ocr_module_version
- 0.0.13
- Ocr_parameters
- -l eng
- Orig_md5
- 53bf0b31343a9e108bdb64a3456efb75
- Page_number_confidence
- 96.55
- Pages
- 262
- Ppi
- 300
- Rights
- This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
- Scanner
- Internet Archive Python library 1.8.1
- Service
- Commander, United States Navy
- Type
- Thesis
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