Add to ORKGTransonic flutter analysis of dynamically and elastically scaled models of sweptback, tapered, all-movable horizontal tail of X-15 aircraf
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
A transonic and a supersonic flutter investigation of 1/2-size models of the all-movable canard surf...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Transonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal ta...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
Flutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraf
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
The flutter model represented the aft fuselage and empennage of a proposed supersonic transport airp...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
A transonic flutter investigation has been made of models of the T-tail of the Blackburn NA-39 airpl...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
Pitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and...
Wind-tunnel tests of the T-tail of a wide-body jet airplane were made at Mach numbers up to 1.02. Th...
"Panel flutter tests were conducted on two-full scale vertical stabilizers of the X-15 airplane at a...
A 1/20-size, low-speed flutter model of the SCAT-15F complete airplane was tested on cables to simul...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
A transonic and a supersonic flutter investigation of 1/2-size models of the all-movable canard surf...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Transonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal ta...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
Flutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraf
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
The flutter model represented the aft fuselage and empennage of a proposed supersonic transport airp...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
A transonic flutter investigation has been made of models of the T-tail of the Blackburn NA-39 airpl...
An experimental and analytical study was made of the transonic flutter characteristics of a superson...
Pitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and...
Wind-tunnel tests of the T-tail of a wide-body jet airplane were made at Mach numbers up to 1.02. Th...
"Panel flutter tests were conducted on two-full scale vertical stabilizers of the X-15 airplane at a...
A 1/20-size, low-speed flutter model of the SCAT-15F complete airplane was tested on cables to simul...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
A transonic and a supersonic flutter investigation of 1/2-size models of the all-movable canard surf...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...