| 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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