Summary
New concepts for guiding and controlling the flight of projectiles in the hypersonic speed regime up to Mach number 10 or more, such as the missile’s outer contour deformation are under investigation for future applications. Strong lateral forces can be obtained if the deformation takes place at the projectile’s nose. For this purpose a flat ramp with ramp angles between 15 deg and 18 deg was machined on conical nose models of 20 deg half angle to create a cone asymmetry. With these models differential interferometry flow visualisations, surface pressure and heat transfer measurements were performed at Mach number 4.6 and 7 km altitude atmospheric conditions at the ISL’s shock tunnel STB to examine the resulting flow around the asymmetric cone model.
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References
F. Seiler, J. Srulijes, H. Lehr, Verfahren zur Steuerung eines Überschallflugkörpers sowie Überschallflugkörper, Deutsche Patentschrift Nr. 198 39 493, Deutsches Patent-und Markenamt, 1998
F. Seiler, U. Werner, G. Patz, Ground testing facility for Modelling Real Projectile Flight Heating in Earth Atmosphere, Journal of Thermophysics, Vol. 16, Nr. 1, January-March 2002
H. Oertel, Wârmeiibergangsmessungen, in “Kurzzeitphysik”, Springer Verlag, Wien-New York, 1967
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© 2004 Springer-Verlag Berlin Heidelberg
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Seiler, F., Srulijes, J. (2004). Pressure and heat flux measurements at the surface of an asymmetric cone at Mach number 4.6 in ISL’s shock tunnel STB. In: Breitsamter, C., Laschka, B., Heinemann, HJ., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics IV. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 87. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-39604-8_16
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DOI: https://doi.org/10.1007/978-3-540-39604-8_16
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-53546-8
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