A method for determining the maximum thickness position for minimum wave drag for wings with supersonic edges
By: L. M. Sheppard.
Contributors: Aeronautical Research Laboratories (Australia)
Series: Aeronautical Research Laboratories. Technical note -- HSA TN12
Publisher: Dept. of Supply, Research and Development Branch, Aeronautical Research Laboratories
Published: 1954
Place of publication: Salisbury, South Australia
Notes: Bibliography : p. 8.