Identifiers: B-70. Model characteristics, flutter speeds, frequencies, test conditions and other data pertinent to flutter evaluation of the B-70 configurations under consideration are presented. The data accumulated have been used to specify stiffness levels required to prevent flutter of the XB-70 Air Vehicle. (Author)
Summary of XM-70 Flutter Model Tests from 1 March 1958 to 20 May 1960 NAA(North American Aviation) Designation NA-267 AF Designation XB-70
1960
10 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Jet bombers , Aerodynamic characteristics , Aerodynamic configurations , Canard configuration , Data , Delta wings , Flaps(Control surfaces) , Flutter , Model tests , Stabilizers (Horizontal tail surface) , Subsonic flow , Transonic characteristics , Wind tunnel models , B-70 aircraft
DESIGNATION DEVICE AND DESIGNATION METHOD OF TRAVEL ROUTE
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