Abstract
With a first rotation about φ with the matrix \(M_1^{+ \phi}\) (x →y, eq. (2.1)) and a second about \(- \: \theta\) with the matrix \(M_2^{- \: \theta}\) (x →z, eq. ((2.5)) we obtain, see Fig. 2.12
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References
Hirschel, E.H., Weiland, C.: Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. In: Progress in Astronautics and Aeronautics, AIAA, Reston, Va, vol. 229. Springer, Heidelberg (2009)
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Weiland, C. (2010). Solution of Problems. In: Computational Space Flight Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-13583-5_11
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DOI: https://doi.org/10.1007/978-3-642-13583-5_11
Publisher Name: Springer, Berlin, Heidelberg
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