Rocket-powered model investigation of lift, drag, and stability of a body-tail configuration at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5 degrees

Gillespie, Warren, Jr Dietz, Albert E
naca-rm-l54c04
April 15, 1954


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l54c04.pdf