A supersonic wind tunnel for Mach numbers up to 3.5.
Contributors: Advisory Group for Aeronautical Research and Development. Wind Tunnel and Model Testing Panel.
Series: Agard report -- 70
Publisher: Agard
Published: 1956
Place of publication: Paris
Language: eng
Notes: Presented at the 9th Meeting of the Wind Tunnel and Model Testing Panel, Brussels, August 1956.