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Posts
- Category: Aerodynamics of a Lifting System in Extreme (continued)
- Integral Formulations for Lifting Surfaces in the Extreme Ground Effect
- The Lift-to-Drag Ratio of a Wing in the Ground Effect
- The Aerodynamic Efficiency of a Wing in the Extreme Ground Effect
- A Discussion of a Mathematical Model of PAR with the Coanda Effect
- Margins of Efficiency of PAR Based on a Reentrant Jet Scheme
- Estimate of the Efficiency and the Thrust Recovery of PAR Based on a Reentrant Jet Scheme
- Envelopes of the Efficiency of Power Augmentation for a Scheme with a Reentrant Jet
- Flow of Infinite Width Past a Trailing Edge with a Flap
- Unseparated Flow Near a Trailing Edge with a Flap
- The Model of Flow Past a Leading Edge with a Winglet
- Coanda Flow of Finite Width Past a Deflected Leading Edge
- Unseparated Flows Near Leading and Trailing Edges
- Local Separated Flow Past a Flap (Endplate)
- Reentrant Jet Flow Near the Leading Edge with a Deflected Tip
- Local Flow Problems for Analysis of PAR Mode
- Schematized Flow Models for a Power-Augmented Lifting System
- The Aerodynamic Response of a Lifting System to Aperiodic Perturbations
- An Estimate of the Acceleration of a Lifting Surface in Flight over a Wavy Wall
- The Aerodynamics of a Lifting System Near Curved Ground
- Slotted Wings in the Ground Effect
- A Wing with a Rotating Flap
- . Steady Flow Past a Jet-Flapped Wing of Finite Span
- Nonlinear Steady Flow Problem for a Foil with a Jet Flap
- A Lifting System with a Jet Flap in the Extreme Ground Effect
- The Influence of Endplates, Flaps, and Slots
- Nonlinear Steady Compressible Flow Problem for a Foil
- Compressible Linearized Unsteady Flow Past a Wing of Finite Span
- Steady Linearized Compressible Flow Past a Wing of Finite Span
- Channel Flow in a Compressible Fluid
- Compressible Flow Past a Wing in the Extreme Ground Effect
- Unsteady Perturbation of a Steady Flow
- Unsteady Flow Solutions for a Wing with Endplates
- Steady-State Solutions for Flow Past a Wing with Endplates
- A One-Dimensional Flow Model for a Flying Wing with Endplates
- Nonlinear Flow Problems for a Lifting System in the Extreme Ground Effect
- Three-Dimensional Unsteady Linearized Lifting Flows
- Harmonic Oscillations of a Thin Foil in a Two-Dimensional Flow
- Steady Flow Past a Wing of Arbitrary Aspect Ratio
- A Wing of Small Aspect Ratio in a Steady Linearized Flow
- Two-Dimensional Steady Flow Past a Slightly Curved Foil
- Features of a Linearized Formulation and an Algorithm of the Solution
- . The Linear Theory of a Lifting System Moving Close to the Ground
- A Uniformly Valid Flow Description and Aerodynamic Coefficients
- Matching of Flow Descriptions in Different Regions
- Flows in the Vicinity of Edges
- Flow Above the Lifting System and Its Wake
- Flow Below the Lifting System and Its Wake (Channel Flow)
- Problem Formulation for the Flow Past a Lifting Surface in Proximity to a Solid Boundary
- Numerics: Viscous Flows, Navier—Stokes Solvers
- Numerics: Euler Codes for Unsteady Flows
- Numerics: Euler Codes for Steady Flows
- Asymptotic and Numerical Methods in the Aerodynamics of the Wings-in-Ground Effect
- A Brief Reference on Wing-in-Ground-Effect Craft
- Aerodynamics of a Lifting System in Extreme
- Category: AERODYNAMICS OF THE AIRPLANE
- Control Surfaces on the Tail Unit
- Flaps on the Wing in Compressible Flow
- FLAPS ON THE WING OF FINITE SPAN AND ON THE TAIL UNIT
- Take-off and Landing Devices[36]
- The Flap Wing in Compressible Flow
- THE FLAP WING OF INFINITE. SPAN (PROFILE THEORY)
- Aerodynamic Coefficients of the Flaps and Control Surfaces
- Geometry of the Flaps and Control Surfaces
- AERODYNAMICS OF THE FLAPS AND CONTROL SURFACES
- Interaction of the Vertical Tail. and the Horizontal Tail
- Thus the above conclusions have been confirmed
- Effect of the Wing-Fuselage System on the Vertical Tail
- The Vertical Tail without Interference
- AERODYNAMICS OF THE VERTICAL TAIL
- Influence of the wing on the horizontal tail in supersonic incident flow For
- The Horizontal Tail in Supersonic Incident Flow
- The Horizontal Tail in Subsonic Incident Flow
- The Horizontal Tail in Incompressible Flow
- AERODYNAMICS OF THE HORIZONTAL TAIL
- Geometry of the Tail Surfaces
- AERODYNAMICS OF THE STABILIZERS
- SLENDER BODIES
- The Wing-Fuselage System in Transonic Incident Flow
- The Wing-Fuselage System in Supersonic Incident Flow
- THE WING-FUSELAGE SYSTEM IN COMPRESSIBLE FLOW
- The Wing-Fuselage System in Asymmetric Incident Flow
- The Wing-Fuselage System in Symmetric Incident Flow
- THE WING-FUSELAGE SYSTEM. IN INCOMPRESSIBLE FLOW
- Aerodynamic Coefficients
- Geometry of the Wing-Fuselage System
- AERODYNAMICS OF THE WING - FUSELAGE SYSTEM
- The Fuselage in Subsonic Incident Flow
- THE FUSELAGE IN COMPRESSIBLE FLOW
- The Fuselage in Asymmetric Incident Flow
- The Fuselage in Axial Flow
- THE FUSELAGE IN INCOMPRESSIB LE FLOW
- Forces and Moments on the Fuselage
- AERODYNAMICS OF THE FUSELAGE AND THE WING-FUSELAGE SYSTEM
- Wing of Finite Thickness. in Supersonic Flow
- Inclined Wing in Supersonic Flow
- Method of Singularities for Supersonic Flow
- Method of Cone-Symmetric Supersonic Flow
- WING OF FINITE SPAN AT SUPERSONIC INCIDENT FLOW
- Wing of Finite Thickness at Subsonic Incident Flow
- Inclined Wing at Transonic Incident Flow