NASA technical note TN (series). D-4929. Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow [with list of references]; by M. J. Queijo.
Publication Title:
Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow [with list of references]; by M. J. Queijo.
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NASA technical note TN (series). D-4929. Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow [with list of references]; by M. J. Queijo.