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[null,"1.","Record Nr.",null,"UNINA990000620790403321"]
[null,null,"Autore",null,"Capurso, Michele"]
[null,null,"Titolo",null,"SU DI UNA GENERALIZZAZIONE DEL SUOLO DI WIEGHARDT PER LE STRUTTURE DI FONDAZIONE BIDIMENSIONALI,1965 / CAPURSO M."]
[null,null,"Pubbl/distr/stampa",null,"Napoli : I.T.C., 1965"]
[null,null,"Locazione",null,"DINSC"]
[null,null,"Collocazione",null,"07 U/1359"]
[null,null,"Lingua di pubblicazione",null,"Italiano"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Atti dell'Istituto di Tecnica delle Costruzioni dell'Università di Napoli."]
[null,"2.","Record Nr.",null,"UNINA9911006606603321"]
[null,null,"Autore",null,"Etkin Bernard"]
[null,null,"Titolo",null,"Dynamics of Atmospheric Flight"]
[null,null,"Pubbl/distr/stampa",null,"Newburyport, : Dover Publications, 2012"]
[null,null,"ISBN",null,"0-486-14165-9"]
[{"$nulls":4},"1-62198-609-8"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (833 p.)"]
[null,null,"Collana",null,"Dover Books on Aeronautical Engineering"]
[null,null,"Disciplina",null,"629.132/3"]
[null,null,"Soggetti",null,"Aerodynamics"]
[{"$nulls":4},"Stability of airplanes"]
[{"$nulls":4},"Flight"]
[{"$nulls":4},"Mechanical Engineering"]
[{"$nulls":4},"Engineering & Applied Sciences"]
[{"$nulls":4},"Aeronautics Engineering & Astronautics"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Description based upon print version of record."]
[null,null,"Nota di contenuto",null,"Title Page; Copyright Page; Preface; Table of Contents; CHAPTER I - Introduction; TYPES OF PROBLEMS; THE TOOLS OF FLIGHT DYNAMICISTS; CHAPTER 2 - Analytical tools; 2.1 INTRODUCTION; 2.2 VECTOR/MATRIX ALGEBRA; 2.3 LAPLACE AND FOURIER TRANSFORMS; 2.4 APPLICATION TO DIFFERENTIAL EQUATIONS; 2.5 METHODS FOR THE INVERSE TRANSFORMATION; 2.6 RANDOM PROCESS THEORY; 2.7 MACHINE COMPUTATION; CHAPTER 3 - Systems Theory; 3.1 CONCEPTS AND TERMINOLOGY; 3.2 TRANSFER FUNCTIONS; 3.3 AUTONOMOUS LINEAR/INVARIANT SYSTEMS; 3.4 RESPONSE OF LINEAR/INVARIANT SYSTEMS; 3.5 TIME-VARYING AND NONLINEAR SYSTEMS"]
[{"$nulls":4},"CHAPTER 4 - Reference frames and transformations4.1 NOTATION; 4.2 DEFINITIONS OF REFERENCE FRAMES USED IN VEHICLE DYNAMICS; 4.3 DEFINITION OF THE ANGLES; 4.4 TRANSFORMATION OF A VECTOR; 4.5 THE L MATRIX IN TERMS OF ROTATION ANGLES; 4.6 TRANSFORMATION OF THE DERIVATIVE OF A VECTOR; 4.7 TRANSFORMATION OF A MATRIX; CHAPTER 5 - General equations of unsteady motion; 5.1 VELOCITY AND ACCELERATION IN AN ARBITRARILY MOVING FRAME; 5.2 ANGULAR VELOCITIES OF THE SEVERAL REFERENCE FRAMES; 5.3 POSITION, VELOCITY, AND ACCELERATION OF THE VEHICLE MASS CENTER; 5.4 EQUATIONS OF MOTION OF AN ARBITRARY SYSTEM"]
[{"$nulls":4},"5.5 FORCE EQUATIONS IN WIND AXES5.6 FORCE AND MOMENT "]
[{"$nulls":4},"EQUATIONS IN BODY AXES (EULER'S EQUATIONS); 5.7 DISCUSSION OF THE SYSTEM OF EQUATIONS; 5.8 THE FLAT-EARTH APPROXIMATION; 5.9 STEADY STATES; 5.10 THE SMALL-DISTURBANCE THEORY; 5.11 EXACT LINEAR AERODYNAMICS AND THE TRANSFORMED EQUATIONS; 5.13 NONDIMENSIONAL EQUATIONS; 5.14 TRANSFORMS OF THE NONDIMENSIONAL EQUATIONS; 5.15 TRANSFORMATION OF AERODYNAMIC DERIVATIVES FROM ONE BODY-FIXED REFERENCE FRAME TO ANOTHER; CHAPTER 6 - Longitudinal aerodynamic characteristics-part 1; 6.1 THE BASIC LONGITUDINAL FORCES"]
[{"$nulls":4},"6.2 PITCH STIFFNESS AND POSSIBLE CONFIGURATIONS FOR FLIGHT6.3 PITCH STIFFNESS OF A GENERAL CONFIGURATION; 6.4 LONGITUDINAL CONTROL; 6.5 CONTROL HINGE MOMENT; 6.6 INFLUENCE OF A FREE ELEVATOR ON LIFT AND MOMENT; 6.7 THE USE OF TABS; 6.8 CONTROL FORCE TO TRIM; 6.9 CONTROL FORCE GRADIENT; 6.10 MANEUVERABILlTY-ELEVATOR ANGLE AND CONTROL FORCE PER g; CHAPTER 7 - Longitudinal aerodynamic characteristics-part 2; 7.1 BOB WEIGHTS AND SPRINGS; 7.2 INFLUENCE OF HIGH-LIFT DEVICES ON TRIM AND PITCH STIFFNESS; 7.3 INFLUENCE OF THE PROPULSIVE SYSTEM ON TRIM AND PITCH STIFFNESS"]
[{"$nulls":4},"7.4 EFFECT OF STRUCTURAL FLEXIBILITY7.5 GROUND EFFECT; 7.6 C.G. LIMITS; 7.7 LONGITUDINAL AERODYNAMIC DERIVATIVES; 7.8 THE V DERIVATIVES; 7.9 THE q DERIVATIVES; 7.10 THE DERIVATIVES; 7.11 AERODYNAMIC TRANSFER FUNCTIONS; 7.12 THE z DERIVATIVES; 7.13 AEROELASTIC DERIVATIVES; 7.14 SUMMARY OF THE FORMULAE; CHAPTER 8 - Lateral aerodynamic characteristics; 8.1 YAW STIFFNESS (WEATHERCOCK STABILITY); 8.2 YAW CONTROL; 8.3 ROLL STIFFNESS; 8.4 ROLLING CONTROL; 8.5 THE β DERIVATIVES; 8.6 THE p DERIVATIVES; 8.7 THE r DERIVATIVES; 8.8 SUMMARY OF THE FORMULAE; CHAPTER 9 - Stability of steady flight"]
[{"$nulls":4},"9.1 LONGITUDINAL MODES"]
[null,null,null,"Sommario/riassunto","Geared toward upper-level undergrads, graduate students, and practicing engineers, this comprehensive treatment of the dynamics of atmospheric flight focuses especially on the stability and control of airplanes. An extensive set of numerical examples covers STOL airplanes, subsonic jet transports, hypersonic flight, stability augmentation, and wind and density gradients.The equations of motion receive a very full treatment, including the effects of the curvature and rotation of the Earth and distortional motion. Complete chapters are given to human pilots and handling qualities and to flight i"]