Add to ORKGAerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressure tunne
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration
This report presents the results of an investigation in the transonic speed range of the longitudina...
Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speed
Basic pressure measurements on 0.0667-scale model of north american x-15 research aircraft at transo...
Transonic aerodynamic characteristics of supersonic fighter-bomber aircraft model with external fuel...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...
Drag coefficients from modified X-15-2 aircraft configurations at speeds up to Mach 6.
Aerodynamic drag of external fuel tanks attached to X-15-2 airplane at Mach numbers of 1.6 to 2.
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic spee...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration
This report presents the results of an investigation in the transonic speed range of the longitudina...
Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speed
Basic pressure measurements on 0.0667-scale model of north american x-15 research aircraft at transo...
Transonic aerodynamic characteristics of supersonic fighter-bomber aircraft model with external fuel...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...
Drag coefficients from modified X-15-2 aircraft configurations at speeds up to Mach 6.
Aerodynamic drag of external fuel tanks attached to X-15-2 airplane at Mach numbers of 1.6 to 2.
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic spee...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration
This report presents the results of an investigation in the transonic speed range of the longitudina...