Experimental investigation of the DLR-F6 transport configuration in the national transonic facility (invited)

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2008, Pages

  Gatlin, Gregory M ^a,d,e   Rivers, Melissa B ^a,d,e   Goodliff, Scott L ^b,e,f   Rudnik, Ralf ^c   Sitzmann, Martin ^c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Jacobs Sverdrup   (United States)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

^d Mail Stop 267

^e AIAA ^*

^f ROME Group

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMIC DRAG; AVIATION; COMPUTATIONAL FLUID DYNAMICS; DATA VISUALIZATION; NASA; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; TEMPERATURE; TRANSONIC AERODYNAMICS; WIND TUNNELS;

EXPERIMENTAL AERODYNAMICS; EXPERIMENTAL INVESTIGATIONS; GERMAN AEROSPACE CENTERS; LOW TEMPERATURE CONDITIONS; MODEL DEFORMATIONS; REYNOLDS NUMBER EFFECT; SURFACE FLOW VISUALIZATION; WING-BODY CONFIGURATIONS;

FLOW VISUALIZATION;

EID: 85067321551     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6917     Document Type: Conference Paper

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