Free-flight investigation of the drag of a model of a 60 degree delta-wing bomber with strut-mounted siamese nacelles and indented fuselage at Mach numbers from 0.80 to 1.35

Hoffman, Sherwood
naca-rm-l57g29
September 25, 1957


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l57g29.pdf