Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration having a 60 degree delta wing and a high unswept horizontal tail

Peck, Robert F Mitchell, Jesse L
naca-rm-l52k04a
January 05, 1953


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1953/naca-rm-l52k04a.pdf