Self-induced roll oscillation of 45-degree delta wings

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Matsuno, Takashi ^a   Nakamura, Yoshiaki ^a  

^a NAGOYA UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894308360     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Ericsson, L. E., "The Fluid Mechanics of Slender \Ving Rock, " J. Aircmjt, Vol. 21. No. 5, IX+4, pp. X22-328.
2. Levin, D. and Katz,.I., "Dynamic Load Measurements with Delta CVings [Jndergoing Self-Induced Rr-ll Oscillatir)rl, ".J. Aircr. & Vol. 21, 90. 1, 1984, pp. 30-x.
3. Pelletier, A. and Nelson, R. C:., "Dvuarnic: Hehavior of An 800/Go Doilble-Delt, a Wing in Roll, " r\IAA 0X-4353, IWX.
4. Kawazoc, H., Nakamura, Y., One, T., and Iishimaru Y., "Static and Total Pressure Distribut, ions around a Thick De1l. a Wing with Rounded Leading Edge, " A IA A 94-232 1: I W-4.
5. Ueno, M., Matsuno, T. and Nakamura. Y. "linstead) Aerodynamics of Rolling Delta Wings with High. Ibpect Ratio. " AIA. r\ 98-2520, 1998.
6. Ericsson, L. E., "Flow Physics of Critical St, ates for Rolling Delta Wings, ".J. Aircraft, vol. 32, No. 3, 1905, pp. 603-610.