Supersonic flow around a body of small elongation

Supersonic flow around a body of small elongation

Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.

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Veröffentlicht in:Moscow University mechanics bulletin 2009-10, Vol.64 (5), p.123-125
Hauptverfasser: Guvernyuk, S. V., Zubkov, A. F., Pichkhadze, K. M., Finchenko, V. S., Shvets, A. I.
Format: Artikel
Sprache:eng
Schlagworte:
Brief Communications
Classical Mechanics
Physics
Physics and Astronomy
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Beschreibung
Zusammenfassung:Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.
ISSN:0027-1330
1934-8452
DOI:10.3103/S0027133009050057