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Posts
- Category: AERODYNAMICS OF THE AIRPLANE (continued)
- Inclined Wing at Subsonic Incident Flow
- WING OF FINITE SPAN IN SUBSONIC AND TRANSONIC FLOW
- Airfoil of Infinite Span in Hypersonic Flow
- Profile Theory of Transonic Flow
- AIRFOIL OF INFINITE SPAN IN COMPRESSIBLE FLOW (PROFILE THEORY)
- Similarity Rules for Wing Theory at Compressible Flow
- Friction Drag on a Flat Plate. in Compressible Flow
- BASIC CONCEPT OF THE WING IN COMPRESSIBLE FLOW
- WINGS IN COMPRESSIBLE FLOW
- Results of the Teardrop Theory. for Wings of Finite Span
- WING OF FINITE THICKNESS AT ZERO LIFT
- Stability Coefficients of Lateral Motion
- Stability Coefficients of Longitudinal Motion
- FLIGHT MECHANICAL COEFFICIENTS OF THE WING
- Tangential Force and Suction Force
- Computation of Induced Drag
- INDUCED DRAG OF WINGS
- Maximum Lift of Wings
- Nonlinear Wing Theory
- Extended Lifting-Line Theory
- Computation of Total Lift
- LIFT OF WINGS IN INCOMPRESSIBLE FLOW
- Integral Equation for the Circulation Distribution from the Extended Lifting-Line Theory
- Integral Equation for Circulation Distribution from Wing Theory
- WING THEORY BY THE METHOD. OF VORTEX DISTRIBUTION
- Lift Distribution
- Shapes of Actual Wings
- WINGS OF FINITE SPAN IN INCOMPRESSIBLE FLOW
- Boundary-Layer Control on the Wing
- Effect of Reynolds Number on Drag
- INFLUENCE OF VISCOSITY AND BOUNDARY-LAYER CONTROL ON PROFILE CHARACTERISTICS*
- Special Problems of Profile Theory
- Inclined Profile of Finite Thickness
- Symmetric Profiles of Finite Thickness in Chord-Parallel Incident Flow (Teardrop Theory)
- Very Thin Profiles (Skeleton Theory)
- PROFILE THEORY BY THE METHOD OF SINGULARITIES
- Joukowsky Profiles
- Inclined Flat Plate
- PROFILE THEORY BY THE METHOD OF CONFORMAL MAPPING
- Methods of Profile Theory
- Magnitude and Formation of Circulation
- FUNDAMENTALS OF LIFT THEORY
- AIRFOIL OF INFINITE SPAN IN INCOMPRESSIBLE FLOW (PROFILE THEORY)
- Interrelation between the Aerodynamic Forces. and the Modes of Motion of the Airplane
- Aerodynamic Forces and Moments on Aircraft
- AERODYNAMIC BEHAVIOR OF AIRPLANES
- Hysical Properties of the Atmosphere
- PHYSICAL PROPERTIES OF AIR
- AERODYNAMICS OF THE AIRPLANE
- Category: Aerodynamics of V/STOL Flight
- Static Stability and Control of a GEM
- Operation of a GEM over Water
- The GEM in Forward Flight
- Hover Performance
- Ground-effect machines
- The Design of Cascades for a Prescribed Chord wise Pressure Distribution
- The Deflection of a Jet by a Cascade of Airfoils
- Thrust augmentation and deflection of jets from turbo-jet engines
- Increase in Maximum Lift by Suction
- Von Karman Momentum Integral Equation
- Boundary layer control by suction
- Fan-in-Wing Configuration
- The Ducted Propeller at an Angle of Attack
- Design of the Stator
- Power Requirements
- Shroud Design
- Ducted Propeller in Axial Flight
- Ducted propeller and fan-in-wing configurations
- Linearized Theory
- Longitudinal Force
- Behavior of a Wing in a Propeller Slipstream
- Propeller Analysis
- Wings and propellers separately and in combination at high angles of attack
- Thrust and Drag
- The jet flap
- Effect of Sweepback on Flap Performance
- Nose Flaps
- Finite Wings with Flaps
- Two-Dimensional Unpowered Flaps
- Unpowered flaps
- Helicopter Performance
- Effect of Different Helicopter Configurations on the Required Power
- Retreating Blade Stall Limitations
- Blade Element Method for Calculating the Power Required in Forward Flight Including Compressibility and Blade Stall
- Simplified Theory of Forward-Flight
- Forward Flight
- Autorotation
- Vertical Descent
- Special Problems in Hover
- Application of Vortex Theory
- Hovering Performance
- Aerodynamics of the helicopter
- Variation of Induced Velocity with Axial Distance
- Propeller Charts and Empirical Methods
- Design of a New Propeller
- Vortex Theory of Propellers
- Blade Element Theories
- The aerodynamics of propellers
- Approximate Lifting Surface Theory
- Lifting Surface Theory for Slender Wings of Low Aspect Ratio