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Posts
- Category: The Art of the Helicopter (continued)
- Category: THEORETICAL AERODYNAMICS
- The Phugoid Oscillation
- Phugoid Motion
- Banked Turn
- Straight Side-Slip
- Sudden Increase of Incidence
- Straight Horizontal Flight
- Gliding
- Stalling
- Linear Flight
- Simple Flights
- Pressure Coefficient
- Compressible Subsonic Flow
- Flow over a Wave-Shaped Wall 507404511
- Equation for the Streamlines from Kinematic Flow Condition
- Existence of Characteristics in a Physical Problem
- General Linear Solution for Supersonic Flow
- Application of Thin Aerofoil Theory
- . Thin Aerofoil Theory
- Shock-Expansion Theory
- The Prandtl-Meyer Function
- Supersonic Expansion by Turning
- Supersonic Compression
- Weak Oblique Shocks
- Supersonic Flow over a Wedge
- Relation between в and в
- Oblique Shock Relations
- Oblique Shock and Expansion Waves
- Change of Total Pressure across a Shock
- The Normal Shock Relations for a Perfect Gas
- Normal Shock Waves
- Moving Disturbance
- The Prandtl-Glauert Rule
- Application to Bodies of Revolution and Fuselage
- Application to Wings of Finite Span
- Gothert Rule
- Three-Dimensional Flow: The Gothert Rule
- Hypersonic Similarity
- Use of Karman Rule
- The von Karman Rule for Transonic Flow
- Analogy Version I
- Prandtl-Glauert Rule for Supersonic Flow: Versions I and II
- The Streamline Analogy (Version III): Gothert’s Rule
- The Indirect Problem (Case of Equal Potentials): P-G Transformation - Version II
- Two-Dimensional Flow: Prandtl-Glauert Rule for Subsonic Flow
- Similarity Rule
- Pressure Coefficient
- Potential Equation for Bodies of Revolution
- Linearization of the Potential Equation
- The General Potential Equation for Three-Dimensional Flow
- Crocco’s Theorem
- Compressible Flow Equations
- Discharge from a Reservoir
- Isentropic Flow
- Thermodynamics of Compressible Flows
- Compressible Flows
- Lifting Surface
- Aerofoils of Small Aspect Ratio
- Calculation of the Downwash Velocity
- Rectangular Aerofoil
- Blenk's Method
- The Induced Lift
- . Munk’s Theorem of Stagger
- Lifting Surface Theory
- Yawing Moment
- Rolling Moment
- Lift on the Aerofoil
- The Rectangular Aerofoil
- The Lift for Elliptic Loading
- Problem II
- Change of Aspect Ratio with Incidence
- Lift and Drag for Elliptical Loading
- Elliptic Loading
- Effect of Downwash on Incidence
- Lancaster - Prandtl Lifting Line Theory
- Condition for Vortex Drag Minimum
- Characteristics of a Simple Symmetrical Loading - Elliptic Distribution
- Downwash
- Finite Aerofoil Theory
- Using Panel Methods
- Pressure Distribution around a Circular Cylinder by Source Panel Method
- The Vortex Panel Method
- Coefficient of Pressure
- Panel Method
- Effect of Operating a Flap
- Jet Flap
- Hinge Moment Coefficient
- Flapped Aerofoil
- Lift, Pitching Moment and Center of Pressure Coefficients for a Thin Aerofoil
- The General Thin Aerofoil Section
- Lift, Pitching Moment, and the Center of Pressure Location for Circular Arc Aerofoil
- The Circular Arc Aerofoil
- The Aerodynamic Coefficients for a Flat Plate
- Solution of the General Equation
- General Thin Aerofoil Theory
- Thin Aerofoil Theory
- Exercise Problems
- Line Vortex