Add to ORKGHorizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft mode
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...
Results of an investigation of the static longitudinal stability and control characteristics of an a...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An investigation was made in the high Mach number test section of the Langley Unitary Plan wind tunn...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
An experimental investigation of the static longitudinal, lateral, and directional stability charact...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
Static stability and control characteristics of aircraft model with tail surfaces outboard of wing t...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Experimental investigations have been conducted to determine the effect of wing vertical position an...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
A low-speed investigation was made on a highly-swept arrow-wing model to determine the effect of win...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...
Results of an investigation of the static longitudinal stability and control characteristics of an a...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An investigation was made in the high Mach number test section of the Langley Unitary Plan wind tunn...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
An experimental investigation of the static longitudinal, lateral, and directional stability charact...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
Static stability and control characteristics of aircraft model with tail surfaces outboard of wing t...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Experimental investigations have been conducted to determine the effect of wing vertical position an...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
A low-speed investigation was made on a highly-swept arrow-wing model to determine the effect of win...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...