Add to ORKGWind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tail surface
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...
Transonic flutter boundaries are presented for two simple, 72 deg. sweep, low-aspect-ratio wing mode...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
Flutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraf
Wind-tunnel tests of the T-tail of a wide-body jet airplane were made at Mach numbers up to 1.02. Th...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
A transonic flutter investigation has been made of models of the T-tail of the Blackburn NA-39 airpl...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
Transonic flutter characteristics of three geometrically similar delta-wing models were experimental...
A transonic and a supersonic flutter investigation of 1/2-size models of the all-movable canard surf...
Transonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal ta...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Flutter investigation of very low aspect-ratio flat-plate surfaces at subsonic and supersonic spee
The flutter model represented the aft fuselage and empennage of a proposed supersonic transport airp...
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...
Transonic flutter boundaries are presented for two simple, 72 deg. sweep, low-aspect-ratio wing mode...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
Flutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraf
Wind-tunnel tests of the T-tail of a wide-body jet airplane were made at Mach numbers up to 1.02. Th...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
A transonic flutter investigation has been made of models of the T-tail of the Blackburn NA-39 airpl...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
Transonic flutter characteristics of three geometrically similar delta-wing models were experimental...
A transonic and a supersonic flutter investigation of 1/2-size models of the all-movable canard surf...
Transonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal ta...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Flutter investigation of very low aspect-ratio flat-plate surfaces at subsonic and supersonic spee
The flutter model represented the aft fuselage and empennage of a proposed supersonic transport airp...
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...
Transonic flutter boundaries are presented for two simple, 72 deg. sweep, low-aspect-ratio wing mode...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...