Hypersonic Curved Compression Inlet and Its Inverse Design by Kunyuan Zhang (Eng
211,21 €
By Kunyuan Zhang. Author Kunyuan Zhang. - Features and Drag Reduction Analysis of Drag in Hypersonic Inlet. The concept of supersonic inlet curved compression discussed originated from the author's research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s.
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