A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2020; you can also visit the original URL.
The file type is application/pdf
.
The computation of the pitch damping stability derivatives of supersonic blunt cones using unsteady sensitivity equations
2019
Advances in Aerodynamics
The numerical methods for computing the stability derivatives of the aircraft by solving unsteady sensitivity equations which was proposed in our previous papers was extended to solve three-dimensional problems in this paper. Both the static and dynamic derivatives of the hypersonic blunt cone undergoing pitching oscillation around a fixed point were computed using the new methods. The predicted static derivative and dynamic derivative were found to be in reasonable agreement with the
doi:10.1186/s42774-019-0018-3
fatcat:7cdic3rabzd6fefqx64amiehhy