Effect of a pilot's canopy on the drag of an NACA RM-2 drag research model in flight at transonic and supersonic speeds

Paul E. Purser
naca-rm-l7l22
Apr 1948


Results of light tests of an NACA RM-2 drag research model equipped with a pilot's canopy are presented for the Mach number range from 0.85 to 1.4. The corresponding Reynolds number range was from 30 X 10(6) to 48 X 10(6) based on the over-all length of the model.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-rm-l7l22.pdf