Computational investigation of the effect of missile control surfaces on F-16 limit cycle oscillation

Authors

• Colin Q. Hanson, Air Force Institute of Technology
• Donald L. Kunz, Air Force Institute of Technology
• Ned J. Lindsley, Air Force Research Laboratory

Document Type

Conference Proceeding

Publication Date

4-8-2013

Comments

The full conference paper is available from AIAA via subscription or purchase, using the DOI link on this page.

DOI

10.2514/6.2013-1836

Source Publication

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Recommended Citation

Hanson, C. Q., Kunz, D. L., & Lindsley, N. J. (2013). Computational investigation of the effect of missile control surfaces on F-16 limit cycle oscillation. <54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA paper 2013-1836. https://doi.org/10.2514/6.2013-1836