Add to ORKGWind tunnel tests to determine effects of wing dihedral angle on aerodynamic characteristics of highly swept fixed-wing configuratio
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
Aerodynamic performance of shuttle-orbiter configuration with variable delta wing geometry in low tu...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
An investigation was conducted in the Langley low turbulence pressure tunnel to determine the effect...
A generalized wind-tunnel model, with canard and wing planforms typical of highly maneuverable aircr...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
An investigation was made in the high Mach number test section of the Langley Unitary Plan wind tunn...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
The experimental longitudinal and lateral-directional stability characteristics of a Langley concept...
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability char...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
An investigation has been conducted at Mach numbers from 2.30 to 4.63 to determine the static aerody...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
Aerodynamic performance of shuttle-orbiter configuration with variable delta wing geometry in low tu...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effect of ...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
An investigation was conducted in the Langley low turbulence pressure tunnel to determine the effect...
A generalized wind-tunnel model, with canard and wing planforms typical of highly maneuverable aircr...
Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the lon...
An investigation was made in the high Mach number test section of the Langley Unitary Plan wind tunn...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
The experimental longitudinal and lateral-directional stability characteristics of a Langley concept...
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability char...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and ...
An investigation has been conducted at Mach numbers from 2.30 to 4.63 to determine the static aerody...
A general research fighter model was tested in the Langley 7- by 10-foot high speed tunnel at a Mach...
Aerodynamic performance of shuttle-orbiter configuration with variable delta wing geometry in low tu...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...