150 |
Lift and rolling moment due to spoilers on wings with trailing-edge flaps deflected at subsonic speeds - extension of Item No. 90030. |
92002 |
150 |
Lift and rolling moment due to spoilers on wings with flaps undeflected at subsonic speeds. |
90030 |
150 |
Program for the calculation of aileron rolling moment and yawing moment coefficients at subsonic speeds. |
88040 |
150 |
Yawing moment coefficient for plain ailerons at subsonic speeds. |
88029 |
150 |
Rolling moment derivative, L sub xi, for plain ailerons at subsonic speeds. |
88013 |
150 |
Rudder sideforce, yawing moment and rolling moment control derivatives at low speeds: Y sub zeta, N sub zeta and L sub zeta. |
87008 |
150 |
Lift and drag due to spoiler operation in the ground run. |
76026 |
150 |
Conversion of lift coefficient increment due to flaps from full span to part span. |
74012 |
150 |
Rate of change of lift coefficient with control deflection for full-span plain controls. |
74011 |
150 |
Rate of change of pitching moment coefficient with control deflection for a plain control in incompressible two-dimensional flow, m sub zero. |
Aero C.08.01.01 |