AIRFLOW STREAMING REVIEWS PLUS

Maximum camber is expressed as a percentage of the chord, with its location as a percentage of the chord aft of the leading edge. The maximum distance of the mean line from the chord line.

Moments and Forces Generated by a PropellerĪ line joining the leading and trailing edges of an aerofoil, equidistant from the upper and lower surfaces.

Effect of a Vertical Gust on the Load Factor.

Methods of Improving Control at Transonic Speeds.Delaying or Reducing the Effects of Compressibility.Factors Which Affect the Buffet Boundaries.

Pressure Distribution at Transonic Mach Numbers.Influence of Temperature on Mach Number at a Constant Flight Level and IAS.Variation of TAS with Altitude at a Constant Mach Number.Effect on Mach Number of Climbing at a Constant IAS.Effect of Weight, Altitude and Temperature.Contribution of the Aeroplane Components.Graphic Presentation of Static Longitudinal Stability.Effect of Frost and Ice on the Aircraft.Choice of Flap Setting for Take-off, Climb and Landing.

AIRFLOW STREAMING REVIEWS PLUS

Trailing Edge Plus Leading Edge Devices.Drag and Pitching Moment of Leading Edge Devices.The Effect of Mass and Balance on Spins.Stall and Recovery Characteristics of Canards.Warning to the Pilot of Icing-induced Stalls.Effect of Wing Contamination on Stall Speed.Effect of Mach Number (Compressibility) on Stall Speed.Effect of Landing Gear on the Stall Speed.Effect of High Lift Devices on Stall Speed.Basic Stall Requirements (EASA and FAR).Use of Flight Controls Close to the Stall.The Effect of Configuration on Total Drag.The Effect of Aircraft Gross Weight on Total Drag.Effect of Aircraft Weight on Minimum Flight Speed.International Standard Atmosphere (ISA).

Airflow streaming reviews