Kantrowitz limit (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Kantrowitz limit" in English language version.

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books.google.com

Curran, E. T.; Murthy, S. N. B. (2001-01-01). Scramjet Propulsion. AIAA. ISBN 9781600864414.

Van Wie, D; Kwok, F; Walsh, R (July 1996). "Starting characteristics of supersonic inlets". AIAA 96-2914. doi:10.2514/6.1996-2914. The ability of the classical Kantrowitz limit to predict the restart contraction ratio was assessed, and it was shown to be applicable for the hard unstart/restart configurations.

Kantrowitz, Arthur; duP, Coleman (May 1945). "Preliminary Investigation of Supersonic Diffusers" (PDF). Advance Confidential Report L5D20. Archived (PDF) from the original on October 20, 2016.

Molder, Sannu. "Hypersonic Air Intake Design for High Performance and Starting" (PDF). Department of Mechanical Engineering, McGill University. Quebec: NATO.

Musk, Elon (August 12, 2013). "Hyperloop Alpha" (PDF). SpaceX. pp. 3–4. Archived from the original (PDF) on January 28, 2016. Retrieved August 14, 2013.

Kantrowitz, Arthur; duP, Coleman (May 1945). "Preliminary Investigation of Supersonic Diffusers" (PDF). Advance Confidential Report L5D20. Archived (PDF) from the original on October 20, 2016.
Musk, Elon (August 12, 2013). "Hyperloop Alpha" (PDF). SpaceX. pp. 3–4. Archived from the original (PDF) on January 28, 2016. Retrieved August 14, 2013.