Flight investigation of the effect of a propulsive jet positioned according to the transonic area rule on the drag coefficients of a single-engine delta-wing configuration at Mach numbers from 0.83 to 1.36

Judd, Joseph H Falanga, Ralph A
naca-rm-l56a16
April 13, 1956


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1956/naca-rm-l56a16.pdf