Abstract
a) We find from Table B.1 with linear interpolation \(\rho_\infty = 1.64{\cdot}10^{-5}\) kg/m3 and T ∞ = 196.7 K. From q ∞ = 0.5\(\rho_\infty{v}^2_\infty\) we obtain v ∞ = 7,648.1 m/s. The speed of sound is a ∞ = \((\gamma RT_\infty)^{0.5}\). With R = 287.06m2/s2K, Table C.1, and γ = 1.4, we get a ∞ = 281.1 m/s and M ∞ = 27.2.
b) We find from Table B.1 \(\rho_\infty = 9.89{\cdot}10^{-5} kg/m^3\) and T ∞ = 222.3 K and obtain v ∞ = 6, 198.6 m/s, a = 298.9 m/s and M ∞ = 20.7.
Access provided by Autonomous University of Puebla. Download to read the full chapter text
Chapter PDF
Keywords
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.
References
Schwartz, M.: New Materials, Processes, and Methods Technology. Taylor and Francis, Boca Raton (2006)
Hirschel, E.H.: Basics of Aerothermodynamics, Progress in Astronautics and Aeronautics, AIAA, Reston, Va, vol. 204. Springer, Heidelberg (2004)
Rights and permissions
Copyright information
© 2009 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Hirschel, E.H., Weiland, C. (2009). Solution Guide and Solutions of the Problems. In: Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-89974-7_11
Download citation
DOI: https://doi.org/10.1007/978-3-540-89974-7_11
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-89973-0
Online ISBN: 978-3-540-89974-7
eBook Packages: EngineeringEngineering (R0)