A numerical method for determining the linearised flow over wings at supersonic speeds
By: K. D. Thomson.
Contributors: Aeronautical Research Laboratories (Australia)
Series: Aeronautical Research Laboratories. High Speed Aerodynamics Division. Technical note -- HSA TN20
Publisher: Dept. of Supply, Research and Development Branch, Aeronautical Research Laboratories
Published: 1955
Place of publication: Salisbury, South Australia
Notes: Bibliography: p. 8.