Neil Armstrong class handout on compressible airspeed theory, for Aircraft Flight Testing class at University of Cincinnati, held winter quarter 1977
Neil Armstrong class handout on compressible airspeed theory, for Aircraft Flight Testing class at University of Cincinnati, held winter quarter 1977
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Author
Armstrong, Neil, 1930-2012
Issue Date
2013-11-21
Item Type
Archival Material
Text
Text
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Academic Department
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Subject
Armstrong, Neil, 1930-2012
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Abstract
Description
For Neil Armstrong class handout on airspeed summary, for Aircraft Flight Testing class, see: <a href="http://hdl.handle.net/2374.UC/730956">http://hdl.handle.net/2374.UC/730956</a>
For Neil Armstrong class handout on maneuver margins, for Aircraft Flight Testing class, see: <a href="http://hdl.handle.net/2374.UC/730957">http://hdl.handle.net/2374.UC/730957</a>
For Neil Armstrong class handout on dihedral, for Aircraft Flight Testing class, see: <a href="http://hdl.handle.net/2374.UC/731007">http://hdl.handle.net/2374.UC/731007</a>
Class handout provided by Bob Levo, UC '77 AsE. Mr. Levo provided the following note with the document: <blockquote>"Compressible Airspeed Theory Calculation" defines how to account for the fact that air is compressible and this effect becomes quite noticeable above approximately Mach 0.6 to 0.8. It accounts for the Mach Number effects mentioned in the previous paragraph.</blockquote> (The reference to "previous paragraph" is the note in <a href="http://hdl.handle.net/2374.UC/730956">hdl.handle.net/2374.UC/730956</a>.)
Alternative title from caption
For Neil Armstrong class handout on maneuver margins, for Aircraft Flight Testing class, see: <a href="http://hdl.handle.net/2374.UC/730957">http://hdl.handle.net/2374.UC/730957</a>
For Neil Armstrong class handout on dihedral, for Aircraft Flight Testing class, see: <a href="http://hdl.handle.net/2374.UC/731007">http://hdl.handle.net/2374.UC/731007</a>
Class handout provided by Bob Levo, UC '77 AsE. Mr. Levo provided the following note with the document: <blockquote>"Compressible Airspeed Theory Calculation" defines how to account for the fact that air is compressible and this effect becomes quite noticeable above approximately Mach 0.6 to 0.8. It accounts for the Mach Number effects mentioned in the previous paragraph.</blockquote> (The reference to "previous paragraph" is the note in <a href="http://hdl.handle.net/2374.UC/730956">hdl.handle.net/2374.UC/730956</a>.)
Alternative title from caption