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Posts
- Category: BASIC HELICOPTER AERODYNAMICS (continued)
- Blade Vortex Interaction
- Wake Analysis
- Descending Forward Flight
- Rotor Aerodynamics in Forward Flight
- Testing Procedures
- . Simple Analysis with Fuselage Motion
- Blade Flexibility
- Lag Frequency
- Coriolis Acceleration
- Blade Sailing
- Equivalence of Flapping and Feathering
- Rotor Control
- Flapping Motion
- Rotor Mechanisms for Forward Flight1
- Tip Loss
- Power Approximations
- Blade Mean Lift Coefficient
- Constant Downwash
- Non-uniform Inflow
- Thrust Approximations
- Rotor in Vertical Flight: Blade Element Theory
- Brownout
- Ground Effect
- Wake Analysis Methods
- Complexity of Real Wake
- Summary Remarks on Momentum Theory
- Ideal Autorotation
- Autorotation
- Complete Induced-Velocity Curve
- Wind Tunnel Test Results
- Descent
- Modelling the Streamtube
- Axial Flight
- Figure of Merit
- Non-dimensionalization
- Rotor in Vertical Flight: Momentum Theory and Wake Analysis
- Book Presentation
- The Helicopter from an Engineering Viewpoint
- Post-war Years
- Second World War Era
- First World War Era
- Introduction
- Units
- Preface to Third Edition
- Preface to Second Edition
- Preface to First Edition
- Series Preface
- BASIC HELICOPTER AERODYNAMICS
- Category: Basics of Aero - thermodynamics
- Wall Shear Stress at Attachment Lines
- Symbols and Acronyms
- Dimensions and Conversions
- Constants, Functions, SI Dimensions and Conversions
- Governing Equations for Flow in General Coordinates
- Problems of Chapter 10
- Problems of Chapter 9
- Problems of Chapter 7
- Problems of Chapter 6
- Problems of Chapter 5
- Problems of Chapter 4
- Problems of Chapter 3
- Solution Guide and Solutions of the Problems
- Generic Scramjet Inlet: The Shock-on-Lip Situation
- Flat Plate/Ramp: Length of the Separation Zone
- Reduction of the Turbulent Skin Friction with Side Effects
- Cone-Flow Experiment: Amplification of the Second Instability Mode by Cooling
- Displacement Thickness at a Highly Cooled Wall
- Boundary-Layer Thickness at a Heated Wall
- Examples in Foregoing Chapters
- Qualitative Considerations
- Viscous Thermal Surface Effects: Examples
- Low-Density Effects
- Hypersonic Viscous Interaction
- Nose/Leading-Edge-type (Edney Type IV and III) Interaction
- Ramp-Type (Edney Type VI and V) Interaction
- Shock/Boundary-Layer Interaction Phenomena
- Flow Separation
- Strong Interaction Phenomena
- Turbulence Modeling for High-Speed Flows
- Concluding Remarks
- Transition Models and Criteria
- Prediction of Stability/Instability and Transition in High-Speed Flows
- Free-Stream Disturbances: The Environment
- Surface Properties
- Receptivity Issues
- Relaminarization
- Gortler Instability
- High-Temperature Real-Gas Effects
- Effect of Shock/Boundary-Layer Interaction
- Effect of Three-Dimensional Flow—Cross-Flow Instability
- Attachment-Line Contamination
- Attachment-Line Instability
- Effect of Nose Bluntness—Entropy-Layer Instability
- Cone versus Flat-Plate Boundary-Layer Transition
- Real Flight-Vehicle Effects
- The Influence of the Mach Number and the Thermal State of the Surface
- Inviscid Stability Theory and the Point-of-Inflection Criterion
- Outline of Stability Theory
- Some Basic Observations
- Laminar-Turbulent Transition as Hypersonic Flow Phenomenon