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: AERODYNAMICS, AERONAUTICS, AND FLIGHT MECHANICS (continued)
- LONGITUDINAL CONTROL
- Down wash Angle
- LONGITUDINAL STATIC STABILITY
- COORDINATE SYSTEM—FORCES, MOMENTS, AND VELOCITIES
- STATIC STABILITY AND CONTROL
- THE ART OF ESTIMATING AND SCALING
- ENERGY METHODS FOR OPTIMAL TRAJECTORIES
- OPERATING LIMITATIONS
- RANGE PAYLOAD
- Ground Roll
- Airborne Distance
- MAXIMUM ENDURANCE
- RANGE
- Generalized Power-Required Curve
- RATE OF CLIMB, TIME TO CLIMB, AND CEILINGS
- Balanced Field Length
- Airborne Distance
- Effect of Wind
- Ground Roll
- AIRPLANE PERFORMANCE
- INSTALLATION LOSSES
- Turbofan
- SPECIFIC ENGINE CHARACTERISTICS AND PERFORMANCE
- QUALITATIVE COMPARISON OF THE PERFORMANCE OF TURBOJET, TURBOFAN, AND TURBOPROP ENGINES
- SOME CONSIDERATIONS RELATING TO GAS TURBINE PERFORMANCE
- ENGINE RATINGS
- DESCRIPTION OF THE GAS TURBINE ENGINE
- A BRIEF HISTORY OF THE TURBOJET
- DESIGN OF A NEW PROPELLER
- PROPELLER SELECTION
- Practical Use of Propeller Charts
- Vortex Theory
- Momentum-Blade Element Theory
- Blade Element Theories
- PROPELLER ANALYSIS
- Supercharged Engines
- PISTON ENGINE CHARACTERISTICS
- THE PRODUCTION OF THRUST
- EFFECT OF MACH NUMBER ON THE ZERO LIFT DRAG OF TWO - AND THREE-DIMENSIONAL SHAPES
- Supersonic Leading Edges
- Subsonic Leading Edges
- SUPERSONIC WINGS
- Characteristics of Sweptback Wings
- THREE-DIMENSIONAL WINGS
- Supersonic Flow (Ackeret Theory)
- LINEARIZED COMPRESSIBLE POTENTIAL FLOW
- SUPERSONIC AIRFOILS
- TRANSONIC AIRFOILS
- Expansion Waves
- Oblique Shock Waves
- FUNDAMENTALS OF GAS DYNAMICS
- Subsonic Flow at High Mach Numbers
- LIFT AND DRAG AT HIGH MACH NUMBERS
- LIFT AND DRAG AT HIGH MACH NUMBERS
- TOTAL AIRPLANE DRAG
- DRAG CLEANUP
- Reduction of Skin Friction Drag
- Winglets
- DRAG REDUCTION
- COOLING DRAG
- TRIM DRAG
- EXAMPLE ESTIMATES OF DRAG BREAKDOWN
- DRAG COUNTS 9
- DRAG BREAKDOWN AND EQUIVALENT FLAT-PLATE AREA
- Effective Aspect Ratio
- Calculation of Induced Drag
- INDUCED DRAG
- FORM DRAG
- SKIN FRICTION DRAG
- DRAG
- AIRFOIL CHARACTERISTICS AT LOW REYNOLDS NUMBERS
- Estimation of C^,, for a Complete Airplane Configuration
- Effect of Trim on С^1Х
- The Maximum Lift of a Finite Wing
- The Vortex System for a Wing
- THE LIFTING CHARACTERISTICS OF A FINITE WING
- Powered-Uft Systems
- The Optimum Airfoil for High Lift
- Leading Edge Devices
- Flaps
- MAXIMUM LIFT
- PREDICTION OF AIRFOIL BEHAVIOR
- MODERN AIRFOIL DEVELOPMENTS
- NACA 6-Series
- NACA 1-Series (Series 16)
- AIRFOIL FAMILIES
- AIRFOILS
- THE GENERATION OF LIFT
- The Numerical Calculation of Potential Flow Around Arbitrary Body Shapes
- The Calculation of Flows for Well-Defined Body Shapes
- Biot-Savart Law
- Elementary Flow Functions
- POTENTIAL FLOW
- Determination of True Airspeed
- Bernoulli’s Equation
- Euler’s Equation of Motion
- Conservation of Mass
- Fluid dynamics
- FLUID STATICS AND THE ATMOSPHERE
- FLUID MECHANICS