Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail

Beam, Benjamin H Reed, Verlin D Lopez, Armando E
naca-rm-a55a28
April 25, 1955


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-a55a28.pdf