Airborne shaped sonic boom demonstration pressure measurements with computational fluid dynamics comparisons

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 3473-3507

  Haering Jr , Edward A ^a,e   Murray, James E ^a,e   Purifoy, Dana D ^a,g   Graham, David H ^b,f,h   Meredith, Keith B ^b,h   Ashburn, Christopher E ^c,e   Stucky, Lt Col Mark ^d,i  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

^c ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^d USAF   (United States)

^e Research Aerodynamics   (United States)

^f AIAA   (United States)

^g MS 2802

^h Flight Sciences 9V11/W6 ^*

ⁱ Test Management   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTOUR; SONIC BOOM;

AIRCRAFT MODELS; DATA ACQUISITION; DATABASE SYSTEMS; PRESSURE EFFECTS; PROJECT MANAGEMENT; SUPERSONIC AIRCRAFT;

COMPUTATIONAL FLUID DYNAMICS;

EID: 30744432406     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (28)

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