File:2-01-AERO-Papodopoulos.jpg: Difference between revisions
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== Summary == | == Summary == | ||
Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down. | *Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down. | ||
== Copyright status == | == Copyright status == | ||
[http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg] | *[http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg] | ||
== Source == | == Source == | ||
*Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down. | *Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down. | ||
*[http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg] | *[http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg] |
Latest revision as of 22:06, 2 December 2007
Summary
- Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down.
Copyright status
Source
- Fig. 1. Surface pressure coefficient distribution at Mach 15, 50-degree angle of attack, and elevons at 10 degrees trailing-edge down.
- http://ameslib.arc.nasa.gov/randt/2000/aero/img/2-01-AERO-Papodopoulos.jpg
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