Abstract
Hydrogen is making its appearance on the horizon of supersonic and hypersonic aircraft fuels. The expanding regimes of speed, altitude, and range of aircraft of the 1970’s will grow out of advances in many different technologies. However, hydrogen fuel will be the common design denominator.
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References
B. L. Messinger, “Thermal Management of Lockheed Model 2000 Supersonic Transport,” ASME Paper No. 65-AV-40 (March 1965).
H. A. Berdelman, “Thermal Stresses in the Composite Wall of a Cryogenic Tank,” ASME Paper No. 65-AV-6 (March 1965).
R. T. Parmley and J. J. Brogan, Handbook of Thermal Design Data for Multilayer Insulation Systems, LMSC A742593 (August 11, 1965).
H. O. Croft, Thermodynamics, Fluid Flow and Heat Transmission, McGraw-Hill Book Co., New York (1938).
“Thermal Protection for Liquid-Hydrogen Fuel Tanks in High-Speed Long-Range Aircraft,” RAND Corporation, AD-625 407 (October 1965).
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© 1967 Springer Science+Business Media New York
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Schalla, C.A. (1967). Hydrogen Liquid Level Influence on Aircraft Tank Insulation. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 12. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0489-1_27
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DOI: https://doi.org/10.1007/978-1-4757-0489-1_27
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4757-0491-4
Online ISBN: 978-1-4757-0489-1
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