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- Category: An Introduction to THE THEORY OF. AEROELASTICITY (continued)
- TABULATION OF RESULTS—INCOMPRESSIBLE FLOW
- KtjSSNER-SCHWARZ’ GENERAL SOLUTION
- AIRFOIL PERFORMING VERTICAL-TRANSLATION AND ROTATIONAL OSCILLATIONS[35]
- THE FORM OF THE ACCELERATION POTENTIAL
- GENERAL EQUATIONS
- OSCILLATING AIRFOILS IN TWO-DIMENSIONAL. INCOMPRESSIBLE FLOW
- METHODS OF SOLVING THIN-AIRFOIL PROBLEMS
- BOUNDARY CONDITIONS IN AIRFOIL PROBLEMS
- THE ACCELERATION POTENTIAL OF A PIEZOTROPIC FLUID
- VELOCITY POTENTIAL OF AN IRROTATIONAL FIELD
- VORTICITY AND CIRCULATION
- FUNDAMENTAL EQUATIONS OF AERODYNAMICS
- FUNDAMENTALS OF NONSTATIONARY AIRFOIL. THEORY
- MATHEMATICAL CHARACTERISTICS OF AEROELASTIC PROBLEMS
- AERODYNAMIC OPERATORS
- THE STRUCTURAL OPERATOR
- NATURE OF THE OPERATORS IN AEROELASTICITY
- THE FUNCTIONAL OPERATORS AND THEIR ALGEBRA
- FUNCTIONAL DIAGRAMS
- GENERAL FORMULATION OF AEROELASTIC. PROBLEMS
- FLUTTER
- TRANSFER FUNCTIONS
- RESPONSE TO GUSTS—RIGID AIRPLANE, PITCHING NEGLECTED
- ORDINARY LINEAR DIFFERENTIAL EQUATIONS WITH CONSTANT COEFFICIENTS To solve the equation
- APPLICATIONS OF LAPLACE TRANSFORMATION
- BUFFETING FLUTTER OF A WING
- PREVENTION OF THE STALL FLUTTER
- STALL FLUTTER
- THEORIES OF TAIL BUFFETING
- TAIL-BUFFETING BOUNDARIES
- BUFFETING AND STALL FLUTTER
- 8.7 THE RESPONSE OF A RIGID AIRPLANE TO ATMOSPHERIC TURBULENCES
- THE POWER SPECTRA OF THE EXCITATION AND THE RESPONSE
- STATISTICAL AVERAGES
- THE MEANING OF PROBABILITY AND DISTRIBUTION FUNCTION
- STATISTICAL ASPECTS OF DYNAMIC-STRESS PROBLEMS
- RESPONSE OF AN AIRPLANE TO A GUST OF SPECIFIED PROFILE
- SOME MATHEMATICAL CONCEPTS
- TRANSIENT LOADS, GUSTS
- FLUTTER PREVENTION OR FLUTTER CONTROL
- OTHER FLUTTER PROBLEMS
- LIMITATIONS OF THE THEORY
- CHOICE OF THE GENERALIZED COORDINATES
- FLUTTER OF A THREE-DIMENSIONAL WING
- ENGINEERING FLUTTER ANALYSIS AND. STRUCTURAL DESIGN
- METHODS OF DETERMINING THE CRITICAL SPEEDS
- SOLUTION OF THE FLUTTER DETERMINANT
- FLUTTER OF A TWO-DIMENSIONAL AIRFOIL
- FORCED OSCILLATION DUE TO A PERIODIC EXCITATION
- EQUATIONS OF MOTION OF A TWO-DIMENSIONAL AIRFOIL
- UNSTEADY AERODYNAMIC FORCES ON AN AIRFOIL IN AN INCOMPRESSIBLE FLUID
- THE EFFECT OF STRUCTURAL PARAMETERS OF THE WING ON THE CRITICAL SPEED OF THE TORSION-FLEXURE FLUTTER
- THE STABILITY OF A DISTURBED MOTION
- APPROXIMATE DETERMINATION OF THE CRITICAL SPEED BY GALERKIN’S METHOD
- QUASI-STEADY AERODYNAMIC DERIVATIVES
- TWO-DIMENSIONAL THIN AIRFOILS IN A STEADY FLOW OF AN INCOMPRESSIBLE FLUID
- FUNDAMENTALS OF FLUTTER ANALYSIS
- HISTORICAL REMARKS
- DIMENSIONAL SIMILARITY
- MODEL EXPERIMENTS
- DYNAMIC MASS BALANCING*
- . THE EXTRACTION OF ENERGY FROM AIRSTREAM
- STIFFNESS CRITERIA
- NONDIMENSIONAL PARAMETERS
- BIBLIOGRAPHY
- TWISTING OF PROPELLER BLADES
- THE EFFECT OF ELASTIC DEFORMATION ON THE STATIC LONGITUDINAL STABILITY OF AN AIRPLANE
- TAIL EFFICIENCY
- SWEPT WINGS
- THE EFFECT OF ELASTIC DEFORMATION ON THE LIFT DISTRIBUTION
- THE LIFT DISTRIBUTION ON A RIGID WING
- AILERON REVERSAL—GENERAL CASE
- LOSS AND REVERSAL OF AILERON CONTROL-. TWO-DIMENSIONAL CASE
- GENERAL
- NUMERICAL APPROXIMATIONS — REDUCTION OF INTEGRAL EQUATIONS INTO MATRIX EQUATIONS
- MATRICES
- THE METHOD OF SUCCESSIVE APPROXIMATION
- SOLUTION BY GENERALIZED COORDINATES
- DIVERGENCE OF AN IDEALIZED CANTILEVER WING
- A TWO-DIMENSIONAL EXAMPLE
- DIVERGENCE OF A LIFTING SURFACE
- PREVENTION OF AEROELASTIC INSTABILITIES
- THE H-SHAPED SECTIONS
- THE OSCILLATION OF CYLINDRICAL STRUCTURES IN A FLOW
- THE FLOW AROUND A CIRCULAR CYLINDER
- GENERAL CONSIDERATIONS IN AERODYNAMICS AND THE DIMENSIONLESS COEFFICIENTS
- SOME TYPICAL EXAMPLES OF AEROELASTIC OSCILLATIONS
- SOME AEROELASTIC PROBLEMS IN CIVIL. AND MECHANICAL ENGINEERING
- COUPLED TORSION-FLEXURE OSCILLATIONS OF A CANTILEVER BEAM
- TORSIONAL OSCILLATIONS OF A CANTILEVER BEAM
- COMPLEX REPRESENTATION OF HARMONIC MOTIONS
- NORMAL COORDINATES
- GENERALIZED COORDINATES AND LAGRANGE’S EQUATIONS
- ELEMENTARY AERODYNAMICS
- THE INFLUENCE COEFFICIENTS AND INFLUENCE FUNCTIONS
- THE ELASTIC AXIS
- SHEAR CENTER
- ELEMENTARY BEAM THEORY
- PRELIMINARIES
- the effect of aerodynamic forces