The shock tunnel and its applications to hypersonic flight.
Contributors: Advisory Group for Aeronautical Research and Development. Wind Tunnel and Model Testing Panel.
Series: Agard report -- 144
Publisher: Agard
Published: 1957
Place of publication: Paris
Language: eng
Notes: Presented at the 11th Meeting of the Wind Tunnel and Model Testing Panel, held in Scheveningen, July 1957.