Aircraft Dynamics From Modeling to Simulation

Name: Aircraft Dynamics From Modeling to Simulation
Price: 98.29 USD
Availability: InStock
ISBN: 9780470626672

ISBN-10: 0470626674

ISBN-13: 9780470626672

Edition: 2012

Authors: Marcello R. Napolitano

List price: $274.95

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Description:

Napolitano's Aircraft Dynamics is designed to help readers extrapolate from low level formulas, equations, and details to high level comprehensive views of the main concepts. the text also helps readers with fundamental skills of learning the "basic modeling" of the aircraft aerodynamics and dynamics. The main objective is to organize the topics in "modular blocks" each of them leading to the understanding of the inner mechanisms of the aircraft aerodynamics and dynamics, eventually leading to the development of simple flight simulations schemes.

Book details

List price: $274.95
Copyright year: 2012
Publisher: John Wiley & Sons, Limited
Publication date: 12/20/2011
Binding: Hardcover
Pages: 720
Size: 8.40" wide x 11.20" long x 1.30" tall
Weight: 3.828
Language: English




Aircraft Equations of Motion



Introduction



Reference Frames and Assumptions



Conservation of the Linear Momentum Equations (CLMEs)



Conservation of the Angular Momentum Equations (CAMEs)



Conservation of the Angular Momentum Equations (CAMEs) with Rotor Effects



Euler Angles



Flight Path Equations (FPEs)



Kinematic Equations (KEs)



Gravity Equations (GEs)



Summary of the Aircraft Equations of Motion



Definition of Steady-State and Perturbation Conditions



Aircraft Equations of Motion at Steady-State Conditions



Aircraft Equations of Motion at Perturbed Conditions



Small Perturbation Equations from a Steady-State Level Flight



Summary


References


Student Sample Problems


Problems



Review of Basic Concepts of Aerodynamic Modeling



Introduction



Review of Key Aerodynamic Characteristics for Wing Sections



Wing Planforms and Wing Lift Curve Slope



Review of the Downwash Effect and Effectiveness of Control Surfaces



Determination of the Aerodynamic Center for Wing and Wing1Fuselage



Approaches to the Modeling of Aerodynamic Forces and Moments



Wind Tunnel Analysis



CFD Analysis



Parameter IDentification from Flight Data



Correlation from Wind Tunnel Data and Empirical "Build-Up" Analysis



Summary


References


Student Sample Problems


Problems



Modeling of Longitudinal Aerodynamic Forces and Moments



Introduction



Aircraft Stability Axes



Modeling of the Longitudinal Steady-State Aerodynamic Forces and Moment



Modeling of FAX1



Modeling of FAZ1



Modeling of MA1



Aircraft Aerodynamic Center



Summary of the Longitudinal Steady-State Aerodynamic Forces and Moment



Modeling of the Longitudinal Small Perturbation Aerodynamic Forces and Moments



Modeling of (cD1 , cL1 , cm1)



Modeling of ï¿½cDu , cLu , cmu ï¿½



Modeling of (cDa_ , cLa_ , cma_ ) and (cDq , cLq , cmq)



Summary of Longitudinal Stability and Control Derivatives



Summary


References


Student Sample Problems


Case Study


Short Problems


Problems



Modeling of Lateral Directional Aerodynamic Forces and Moments



Introduction



Modeling of FAY1



Conceptual Modeling of cYï¿½



Mathematical Modeling of cYï¿½



Modeling of cYdA



Modeling of cYdR



Modeling of LA1



Conceptual Modeling of clï¿½



Mathematical Modeling of clï¿½



Modeling of cldA



Modeling of cldR



Modeling of NA1



Conceptual Modeling of cnï¿½



Mathematical Modeling of cnï¿½



Modeling of cndA



Modeling of cndR



Summary of the Lateral Directional Steady-State Force and Moments



Modeling of the Small Perturbation Lateral Directional Aerodynamic Force and Moments



Modeling of cYï¿½_ , cl _ ï¿½ , cn _ ï¿½



Modeling of cYp



Modeling of clp



Modeling of cnp



Modeling of cYr



Modeling of clr



Modeling of cnr



Summary of Longitudinal and Lateral Directional Aerodynamic Stability and Control Derivatives



Final Overview and Ranking of the Importance of the Aerodynamic Coefficients



Summary of the Modeling of the Longitudinal and Lateral-Directional Aerodynamic Forces and Moments


References


Student Sample Problems


Case Study


Short Problems


Problems



Review of Basic Aircraft Performance and Modeling of Thrust Forces and Moments



Introduction



Review of Different Aircraft Propulsion Systems



Piston Engine (Propeller) Aircraft Engines



Turboprop Aircraft Engines



Turbojet Aircraft Engines



Turbofan Aircraft Engines



Ramjet Aircraft Engines



Review of Basic Aircraft Performance



Power at Level Flight



Maximum Aerodynamic Efficiency



Minimum Aerodynamic Drag



Minimum Power Required



Determination of Power Required



Determination of Power Available



Modeling of the Thrust Forces and Moments



Modeling of the Steady-State Thrust Forces and Moments



Modeling of the Small Perturbation Thrust Forces and Moments



Summary


References


Student Sample Problems


Problems



Aircraft Stability and Design for Trim Conditions



Introduction



Concept of Aircraft Stability



Criteria for Aircraft Static Stability



Static Stability Criteria #1 (SSC #1)



Static Stability Criteria #2 (SSC #2)



Static Stability Criteria #3 (SSC #3)



Static Stability Criteria #4 (SSC #4)



Static Stability Criteria #5 (SSC #5)



Static Stability Criteria #5, #6, and #7 (SSC #5, SSC #6, SSC #7)



Static Stability Criteria #9 (SSC #9)



Static Stability Criteria #10 (SSC #10)



Longitudinal Analysis of Steady-State Straight Flight



Lift Chart and Trim Diagram



Lift Chart



Trim Diagram



Trim Diagrams for Different Classes of Aircraft



Trim Diagrams for Thrust Axis Above/Below Center of Gravity



Lateral Directional Analysis of Steady-State Straight Flight



Summary


References


Student Sample Problems


Problems



Solution of the Aircraft Equations of Motion Based on Laplace Transformations and Transfer Functions



Introduction



Application of Laplace Transformations to the Longitudinal Small Perturbation Equations



RouthHurwitz Analysis of the Longitudinal Stability



Longitudinal Dynamic Modes: Short Period and Phugoid



Solution of the Longitudinal Equations



Short Period Approximation



Phugoid Approximation



Summary of the Longitudinal Equations



Application of Laplace Transformations to the Lateral Directional Small Perturbation Equations



RouthHurwitz Analysis of the Lateral Directional Stability



Lateral Directional Dynamic Modes: Rolling, Spiral, and Dutch Roll



Solution of the Lateral Directional Equations



Rolling Approximation



Summary of Lateral Directional Equations



Sensitivity Analysis for the Aircraft Dynamics



Short Period Sensitivity Analysis



Phugoid Sensitivity Analysis



Sensitivity Analysis for the Lateral Directional Parameters



Summary


References


Student Sample Problems


Problems



State Variable Modeling of the Aircraft Dynamics



Introduction



Introduction to State Variables for Nonlinear Systems



Introduction to State Variables for Linear/Linearized Systems



State Variable Modeling of the Longitudinal Dynamics



State Variable Modeling of the Lateral Directional Dynamics



Augmentation of the Aircraft State Variable Modeling



Modeling of the Altitude ï¿½hï¿½



Modeling of the Flight Path Angle ï¿½?ï¿½



Modeling of the Engine Dynamics



Modeling of the Actuator Dynamics



Modeling of the Atmospheric Turbulence



Summary of State Variable Modeling of the Aircraft Dynamics



Summary


References


Student Sample Problems


Problems



Introduction to Modern Flight Simulation Codes



Introduction



Introduction to the Flight Dynamics & Control (FDC) Toolbox



Equations of Motion within the FDC Simulation Environment



FDC Modeling of Beaver Aerodynamic Forces and Moments



Alternative Approach for FDC Modeling of Aerodynamic Forces and Moments



Case Study #1: FDC Modeling of Look-Up Tables Based Aerodynamic Coefficients



FDC Modeling of the Gravity Force



FDC Modeling of the Atmospheric Turbulence Force



FDC Modeling of the Beaver Propulsive Forces and Moments



Case Study #2: FDC Modeling of Propulsive Forces and Moments



Auxiliary FDC Blocks



Additional FDC Blocks



Introduction to the Aerospace Blockset by Mathworks



General Organization of the Aerospace Blockset



Introduction to the Environment Library



Introduction to the Flight Parameters Library



Introduction to the Equations of Motion Library



Introduction to the Aerodynamics Library



Introduction to the Propulsion Library



Introduction to the Utilities Library



Introduction to the Mass Properties Library



Introduction to the Actuators Library



Introduction to the GNC and Animation Libraries



Introduction to AIRLIB



AIRLIB's Strucure



Generic Aircraft Model: Continuous-time Block



Generic Aircraft Model: Discrete-time Block



Collection of Aircraft Models



Alternative Model Implementation



Additional Tools within AIRLIB: The Function 'air3m'



Additional Tools within AIRLIB: The Function 'ab2dv'



Summary


References


Student Sample Problems



Pilot Ratings and Aircraft Handling Qualities



Introduction



Aircraft Flight Envelope



Levels of Aircraft Flying Qualities: Cooper-Harper Pilot Rating



Aircraft Control Authority



Pilot Workload



Pilot Compensation



Levels of Flying Qualities



Classes of Aircraft



Classification of Aircraft Maneuvers and Mission Profile



Flying Quality Requirements for the Longitudinal Dynamics



Longitudinal Control Forces



Requirements for the Damping for the Phugoid Mode



Requirements for the Short Period Mode



Flying Quality Requirements for the Lateral Directional Dynamics



Lateral Directional Control Forces



Requirements for the Dutch Roll Mode



Requirements for the Spiral Mode



Requirements for the Rolling Mode



Requirements for the Roll Control Effectiveness



Additional Requirements for Steady Sideslips



Summary


References



Review of Useful Topics



Review of Vector Operations



Review of Matrix Operations



Review of Center of Gravity and Inertial Properties



Review of Application of Laplace Transform to Linear Constant Coefficients Differential Equations



Review of First and Second Order Systems



Review of Standard Atmospheric Model



Data for Different Aircraft



Introduction



Aircraft 1-Cessna 182



Aircraft 2-Cessna 310



Aircraft 3-Beech 99



Aircraft 4-Cessna T37-A



Aircraft 5-Cessna 620



Aircraft 6-Learjet 24



Aircraft 7-Boeing 747-200



Aircraft 8-SIAI Marchetti S-211



Aircraft 9-Lockheed F-104



Aircraft 10-McDonnell Douglas F-4


Reference



Detailed Drawings for Different Aircraft



Introduction



Aircraft 1-Aeritalia Fiat G-91



Aircraft 2-Beech 99



Aircraft 3-Boeing B52



Aircraft 4-Boeing B727-200



Aircraft 5-Boeing B737-600



Aircraft 6-Boeing B747-200



Aircraft 7-Boeing B757-200



Aircraft 8-Boeing B767-200



Aircraft 9-Cessna Citation CJ3



Aircraft 10-Cessna T37



Aircraft 11-General Dynamics F-16



Aircraft 12-Grumman F-14



Aircraft 13-Learjet 24



Aircraft 14-Lockheed F-104



Aircraft 15-Lockheed F-22



Aircraft 16-Lockheed L-1011



Aircraft 17-McDonnell Douglas C-17



Aircraft 18-McDonnell Douglas DC-8



Aircraft 19.1-McDonnell Douglas DC-9 Series 10



Aircraft 19.2-McDonnell Douglas DC-9 Series 30



Aircraft 19.3-McDonnell Douglas DC-9 Series 40



Aircraft 19.4-McDonnell Douglas DC-9 Series 50



Aircraft 20-McDonnell Douglas DC-10



Aircraft 21-McDonnell Douglas F-4



Aircraft 22-McDonnell Douglas F-15



Aircraft 23-Rockwell B-1



Aircraft 24-SIAI Marchetti S211



Aircraft 25-Supermarine Spitfire


Index