Light Airplane and Glider Static and Dynamic Stability. The Aircraft Maneuvrability / Vittorio PAJNO

Titre : Light Airplane and Glider Static and Dynamic Stability. The Aircraft Maneuvrability : Basic Theory and Calculation Examples Type de document : texte imprimé Auteurs : Vittorio PAJNO, Auteur Editeur : Roma : IBN Editore Année de publication : 2015 Importance : 179 p. ISBN/ISSN/EAN : 978-88-7565-217-3 Note générale : Contents Foreword Introduction Appendix Bibliography Catégories : Avions:Stabilité Planeurs (aéronautique):Conception et construction Planeurs (aéronautique):Pilotage Index. décimale : 629.13 Aéronautique : Appareils, installation, technique de la navigation, pilotage Résumé : Static Stability Analysis Maneuvrable Stability Dynamic Stability Longitudinal and Lateral Dynamic Stability The Quartic Equation Solution Control System Design Elevator Required for Landing Stick Forces for Trim and Stick Force Per "G" Balancing of Control Surfaces CALCULATION EXAMPLES CONTENT Mean aerodynamic Chord Calculation V6 "Kite" C.G. Baricentric Moment of Inertia for V6 "Kite" Static Margins Trim Cases and Stick Forces Per "g" Stick Forces as a Function of Vi Stick Angle with and without Flaps Longitudinal Dynamic Stability of Aircraft Writing Quartic Equations Lateral Dynamic Stability of Aircraft Lateral Quartic Equations The Quartic Equation Solution Design of Aileron Control Surfaces Design of Rudder Control Surfaces Elevator Required for Landing Stick Movements Per "g" Static Equilibration of Mobile Surfaces Graphic Meaning of the Static Margin Effect of Mechanical Device in the Elevator Circuit CONCLUSION

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Code-barres	Cote	Support	Localisation	Section	Disponibilité
B00014680	629.13 PAJ	Ouvrage	BIBLIOTHÈQUE - ACCÈS LIBRE	600 - Sciences appliquées - Technologie	Disponible

Sailplane Design Example : Design Calculation Example. Structural Dimensioning. Technical Specifications - Design Rules / Vittorio PAJNO

Titre : Sailplane Design Example : Design Calculation Example. Structural Dimensioning. Technical Specifications - Design Rules Type de document : texte imprimé Auteurs : Vittorio PAJNO, Auteur Editeur : Roma : IBN Editore Année de publication : 2016 Importance : 315 p. ISBN/ISSN/EAN : 978-88-7565-257-9 Note générale : Content Foreword Introduction Reference Documents Catégories : Planeurs (aéronautique):Conception et construction Index. décimale : 629.13 Aéronautique : Appareils, installation, technique de la navigation, pilotage Résumé : Sailplane Construction evolution Photos SECTIONS Sample Sailplane Drawing and Calculation List Sample Sailplane Data Fuselage Wetted Surface Area Polar Calculation Polar with Airbrakes Open V-N Diagrams Gust Envelope Determination Tow Speed Lift Distribution. Shrenk's Method Mass Forces Determination and Distribution Wing Torsion MT Variation due to Wing "P" and "Q" Wing Torsion Design Consideration Wing Torsion due to Aileron Manœuvre Ailerons Loads Airbrakes Loads Wing Fitting Loads The M.A.C. and M.G.C.Calculation Sailplane Weights and Pitching Moment of Inertia The Pitching Moment of Inertia and Jg Calculation Inertia Moments about the Three Axes: X, Y, Z C.G. Excursion Horizontal Tail Loads. BCAR-E Rules Horizontal Tail Loads. "Means of Compliance" as Per EASA CS 22 Rules. Book 2 Horizontal Tail. Gust Loads Manœuvre. Supplementary Loads on the Horiozontal Tail due to Tail Gust Horizontal Tail. Asymmetric Loads Vertical Tail Loads. Load due to the Rudder Rotation Vertical Tail Loads. Yaw Loads Fin Supplementary Loads Control Loads Fuselage Loads Static Stability Analysis of the Controls Landing Gears. Main Gear Reference Distances STRUCTURAL CALCULATION CONTENT SECTION A - Preliminary Weight Calculation SECTION B - Wing Spar Calculations SECTION C - The Wing Skin Weight and Total Weight SECTION D - Airbrake Structural Check SECTION E - Ailerons SECTION F - Auxiliary Spar Calculation SECTION G - Calculation of Wing-Fuselage Fittings SECTION H - Wing Deflection SECTION I - Empennages SECTION K - Structural Check of the Fuselage SECTION L - Fixed and Retractable Landing Gear SECTION M - Landing Gear Retractation Control SECTION N - Balancing Method SECTION O - Laminations SECTION P - Controls SECTION Q - Equipment and Maintenance

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Code-barres	Cote	Support	Localisation	Section	Disponibilité
B00014655	629.13 PAJ	Ouvrage	BIBLIOTHÈQUE - ACCÈS LIBRE	600 - Sciences appliquées - Technologie	Disponible

Sailplane Design : A Guide for Students and Designers / Vittorio PAJNO

Titre : Sailplane Design : A Guide for Students and Designers : From Drafting to Flight Test Type de document : texte imprimé Auteurs : Vittorio PAJNO, Auteur Editeur : Roma : IBN Editore Année de publication : 2018 Importance : 477 p. ISBN/ISSN/EAN : 978-88-7565-092-6 Note générale : Foreword Acknowledgements Contents Appendixes Calculation Examples Catégories : Aérodynamique Planeurs (aéronautique):Conception et construction Vol à voile Index. décimale : 629.13 Aéronautique : Appareils, installation, technique de la navigation, pilotage Résumé : Glider Design and Drafting Materials Flight Mechanics Glider Aerodynamics Stability. Physical Meaning Glider Stability Calculations Glider Dynamic Stability Calculations Airworthiness Requirements Structural Loads Flutter Static Tests Flight Tests Glider Certification Winglet Design

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Code-barres	Cote	Support	Localisation	Section	Disponibilité
B00014687	629.13 PAJ	Ouvrage	BIBLIOTHÈQUE - ACCÈS LIBRE	600 - Sciences appliquées - Technologie	Disponible

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