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- Category: MECHANICS. OF FLIGHT (continued)
- Category: Military
- TOP-10 the most popular military planes and helicopters
- PAK FA and The night hunter will test in 2014-2015
- The Russian Federation army will take advantage of an antihelicopter mine
- The Ministry of Defence of the Russian Federation is put 150 planes and helicopters
- The American military helicopter broke in Gulf of Aden
- Vertical on helicopters
- The Ministry of Defence of the Russian Federation will receive in 2015 of 16 helicopters Ka-52
- The U.S. Air Force will get the new king among helicopters
- Russia sold helicopters on 400 billion rubles
- Naval Forces of the USA will accept technology on alteration of helicopters in bespilotnik
- The Ministry of Defence of the Russian Federation received the upgraded helicopters Mi-8
- Latest Ka-52 for 99 % consists of the Russian components
- More than one hundred new helicopters arrived in the Air Force of Russia for a year
- Category: Model Aircraft Aerodynamics
- DESIGNING NEW AEROFOILS
- Appendix З
- FINDING THE AERODYNAMIC CENTRE OF A WING
- THE ANGLE OF INCIDENCE
- ALLOWANCE FOR PARASITE DRAG
- ASPECT RATIO CORRECTIONS
- THE POWER FACTOR AND L/D RATIO
- WHAT SHOULD THE CAMBER BE?
- WORKING OUT THE LIFT COEFFICIENT
- SYSTEMS OF UNITS
- GYROCOPTERS AND AUTOGYROS
- RETREATING BLADE STALL
- RETREATING BLADE FLOW REVERSAL
- BLADE FLAP
- CYCLIC PITCH CONTROL
- TRANSLATIONAL FLIGHT
- VERTICAL DESCENT: VORTEX RINGS
- VERTICAL CLIMB
- HOVERING
- The helicopter rotor
- GYROSCOPIC EFFECTS
- THE ‘P’ EFFECT
- ENGINE VIBRATION EFFECTS
- BLADE SECTIONS
- REDUCING VORTEX DRAG ON PROPELLERS
- DOWNWASH
- MATCHING PROPELLER TO POWER
- RELATION OF PITCH TO SPEED
- THE ADVANCE RATIO
- VARIABLE PITCH
- . NON-CONSTANT PITCH PROPELLERS
- CONSTANT PITCH
- BLADE LIFT AND PROPELLER THRUST
- PITCH
- THE PROPELLER AS A ROTATING WING SYSTEM
- GENERAL POINTS ARISING FROM THE FROUDE EQUATION
- Propellers
- MASS BALANCING
- FLUTTER
- AIRBRAKES, SPOILERS AND FLAPS
- THE PYLON RACER IN TURNS
- ADVERSE AILERON DRAG
- FLAPS AND AILERONS
- THE ALL-MOVING TAILPLANE
- Control
- SAILPLANES ON THE TOWLINE
- ‘POWER-ON’ STABILITY
- POWER-ON BALANCE
- SPINNING
- RUDDER-STEERED MODELS
- DIHEDRAL
- 12.27 SPIRAL INSTABILITY
- DUTCH ROLL
- WEATHERCOCK OR YAW STABILITY
- SPECIAL PROBLEMS: POWER MODELS ‘GOING FLAT’
- SPECIAL PROBLEMS: SAILPLANE TUCK UNDER
- HOW LARGE A STATIC MARGIN?
- MULTIPLANES AND TANDEMS
- FUSELAGE AND OTHER EFFECTS
- THE STATIC MARGIN
- STATIC AND DYNAMIC STABILITY
- STICK-FREE AND STICK-FIXED STABILITY
- BALANCE WITH NO TAIL
- THE LIFTING TAIL
- BALANCE WITH ZERO TAIL LOAD
- BALANCE WITH A CANARD LAYOUT
- BALANCE WITH A TAIL DOWNLOAD
- TOE THREE AXES
- NEUTRAL STABILITY
- CONTROLLABILITY AND STABILITY
- Trim and stability
- THE WING ANGLE OF INCIDENCE