SACCON forced oscillation tests at DNW-NWB and NASA Langley 14×22-foot tunnel

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Vicroy, Dan D ^a,d   Loeser, Thomas D ^b,e   Schütte, Andreas ^c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b German Dutch Wind Tunnels   (Germany)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

^d NASA LaRC   (United States)

^e DNW NWB   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

MILITARY VEHICLES; NASA; VELOCITY MEASUREMENT; WIND TUNNELS;

COMPUTATIONAL FLUID DYNAMICS METHODS; FORCED OSCILLATION TEST; INTERNATIONAL RESEARCHES; PARTICLE IMAGE VELOCIMETRY MEASUREMENT; STABILITY AND CONTROL; STATE OF THE ART; SURFACE PRESSURES; UNMANNED COMBAT AIR VEHICLES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78649522934     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4394     Document Type: Conference Paper

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