Wind tunnel validation of shaped sonic boom demonstration aircraft design

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 15763-15768

  Graham, David H ^a,d,e   Dahlin, John A ^a,e,f   Page, Juliet A ^b,e,g   Plotkin, Kenneth J ^b,e,g   Coen, Peter G ^c,e,h  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b WYLE LABORATORIES   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d MZ 9V11 W6   (United States)

^e AIAA   (United States)

^f MZ 1S00/W6 ^*

^g Wyle Research Group   (United States)

^h MS 254

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; PRESSURE EFFECTS; WIND TUNNELS;

SHOCK PATTERNS; SONIC BOOM WAVEFORMS; WIND TUNNEL TESTING;

AIRCRAFT;

EID: 30744465318     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-7     Document Type: Conference Paper

References (5)

1. rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV.
2. Carlson, H. W., Mack R. J., Morris O. A., "A Wind tunnel Investigation of the Effect of Body Shape on Sonic Boom Pressure Distributions," NASA TN D-3106, 1965.
3. Morris, O., "Experimental Studies of Sonic Boom Phenomena at High Supersonic Mach Numbers," NASA SP-255, October 29-30, 1970, pp. 193-203.
4. Ferri, A., "Observations on Problems Related to Experimental Determination of Sonic Boom," NASA SP-255, October 29-30, 1970, pp. 277-284.
5. rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV.