Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies. Lees, L. & Kubota, T. Journal of the Aeronautical Sciences, 24(3):195–202, American Institute of Aeronautics and Astronautics (AIAA), March, 1957.
Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies [link]Paper  doi  bibtex   
@article{lees1957,
	title = {Inviscid {Hypersonic} {Flow} {Over} {Blunt}-{Nosed} {Slender} {Bodies}},
	volume = {24},
	url = {https://arc.aiaa.org/doi/abs/10.2514/8.3803},
	doi = {10.2514/8.3803},
	number = {3},
	journal = {Journal of the Aeronautical Sciences},
	publisher = {American Institute of Aeronautics and Astronautics (AIAA)},
	author = {Lees, Lester and Kubota, Toshi},
	month = mar,
	year = {1957},
	keywords = {Air Transportation, Angle of Attack, Drag Coefficient, Guggenheim Aeronautical Laboratory, Hypersonic Speed, Hypersonic Wind Tunnels, Inviscid Hypersonic Flow, Leading Edges, Pressure Coefficient, Shock Wave Interaction},
	pages = {195--202},
}

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