The computation of the pitch damping stability derivatives of supersonic blunt cones using unsteady sensitivity equations

Author:

Guo Chenxi,Ren Yu-xinORCID

Funder

National numerical wind tunnel project

Publisher

Springer Science and Business Media LLC

Reference32 articles.

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3. Bryan GH (1911) Stability in aviation. Macmillan, New York

4. Tobak M (1954) On the use of indicial function concept in the analysis of unsteady motions of wings and wing-tail combinations, NACA Report 1188

5. Tobak M, Schiff LB (1976) On the formulation of the aerodynamic characteristics in aircraft dynamics, NACA TR R-456

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