Our heavyweight helicopter equal in the world does not have
In Rostov started production of the most load-lifting rotary-wing car The Russian holding «Helicopt[...]
Special Recent Posts
In Italy broke experimental tiltrotor
The experimental military man конвертоплан, developed by "August Vestland's" company, brok[...]
The old plane — nonsense, pilots think - there was an attack
In spite of the fact that the main version of crash of the Russian plane of the Kogalymavia company [...]
The Israeli Apache will subject to peeling
The Israeli shock Boeing AH-64 Apache helicopters will undergo "peeling" procedure. As rep[...]
The aviation industry began to move
On Monday against Dubai Airshow air show - the 2015th Deputy Prime Minister Dmitry Rogozin blew up t[...]
Sitemap
Posts
- Category: Model Aircraft Aerodynamics (continued)
- TAIL UNIT DRAG
- WING-FUSELAGE INTERFERENCE
- SAILPLANE FUSELAGES
- UNDERCARRIAGES
- Parasite drag
- FLIGHT TESTING
- EXPLANATION OF APPENDIX 2
- POLAR CALCULATION BY COMPUTER
- THE AIRCRAFT POLAR
- AEROFOIL SELECTION
- APPLICATION OF RESULTS
- CHARTING THE RESULTS
- OTHER WIND TUNNEL EXPERIMENTS
- CORRECTIONS TO RESULTS
- DELICACY OF INSTRUMENTATION
- CALIBRATION
- The wind tunnel
- TURBULATORS ON LAMINAR AEROFOILS
- RESEARCH BY SELIG, DONOVAN AND FRASER
- EPPLER’S RESEARCH
- CAUTIONARY NOTE
- SAILPLANE AEROFOILS, SCALE AND FULL SIZE
- THE LOW DRAG BUCKET
- THE NACA ‘6’ AEROFOILS
- Laminar flow aerofoils
- THE EFFECT OF NOISE
- OTHER FORMS OF TURBULATOR
- BOUNDARY LAYER INVIGORATORS
- TURBULENT FLOW AEROFOILS
- THE EFFECTS OF STRUCTURE AND SURFACE
- SEPARATION BUBBLES
- TURBULATORS
- THE LEADING EDGE RADIUS
- THE CRITICAL REYNOLDS NUMBER OF AEROFOILS
- Ii. Turbulent flow aerofoils
- LOADS IN FLIGHT
- THE AERODYNAMIC CENTRE
- AEROBATIC MODELS
- MO DESIGN OF CAMBER FLAPS
- VARIABLE CAMBER
- CAMBER AND DRAG
- FLAPS AND CONTROLS
- STALL CONTROL BY CAMBER CHANGES
- THE AERODYNAMIC ZERO
- DESIGNING A NEW PROFILE
- AEROFOIL GEOMETRY AND FAMILIES
- Aerofoil sections: і. Camber
- CRESCENT SHAPED WINGS
- WINGLETS AND TIP SAILS FOR MODELS
- DISADVANTAGES OF WINGLETS
- THE COMMERCIAL EQUATION
- WINGLETS
- TAILPLANES AND FINS AS ENDPLATES (see Fig. 6.7, p.74)
- TIP PLATES AND TIP BODIES
- DOWNTURNED WING TIPS
- TIPS FOR SLOW FLIGHT
- TIPS ON FAST FLYING MODELS
- TANDEMS AND CANARDS
- POINTS OF DETAIL
- SWEPT WINGS
- COMPROMISES WITH THE ELLIPSE
- WASH IN
- THE STRONGLY TAPERED WING
- Planform, twist, wingtips and winglets
- STRUCTURAL PROBLEMS
- DOWNWASH AT THE TAIL
- LOW ASPECT RATIO
- ASPECT RATIO AND ROLL RATES
- THE REYNOLDS NUMBER LIMIT
- ASPECT RATIO
- DOWNWASH
- Reducing vortex-induced drag Aspect ratio
- THE EFFECT OF WIND
- THE DRAG BUDGET
- POWER DURATION: VARIABLE TRIM
- POWER DURATION: THE SPIRAL CLIMB
- POWER DURATION MODELS: CLIMBING
- POWER DURATION MODELS: GLIDING
- GLIDERS: THE SPEED TASK
- GLIDERS: BALLAST
- GLIDERS: PENETRATING
- GLIDERS: SOARING
- SPEED MODELS AND RACERS
- Basic model performance problems
- SEPARATION BUBBLES
- LAMINAR SEPARATION
- TURBULENT BOUNDARY LAYERS
- . TRANSITION
- LAMINAR BOUNDARY LAYERS
- THE BOUNDARY LAYER Re NUMBER
- THE REYNOLDS NUMBER
- Scale effect and the boundary layer
- TOTAL DRAG
- VORTEX DRAG
- DRAG, THE LIFT: DRAG RATIO
- CIRCULATION AND THE BOUND VORTEX
- WING CL AND TOTAL CL
- WING LOADING
- AEROFOIL SECTIONS AND LIFT COEFFICIENTS
- ANGLE OF ATTACK AND TRIM