Aircraft Design Concepts
-10%
portes grátis
Aircraft Design Concepts
An Introductory Course
DeLaurier, James
Taylor & Francis Ltd
05/2022
565
Dura
Inglês
9781138033399
15 a 20 dias
1233
Descrição não disponível.
1. Introduction. 2. Aerodynamic Review. 3. Propeller Analysis. 4. Flying Wing (or Tailless Airplanes). 5. Canard Airplanes and Biplanes. 6. Flight Dynamics. 7. Performance. 8. Balloons and Airships. Appendix A. Multhropp Body-Moment Equation. Appendix B. Alternative Swept-Wing Analysis. Appendix C. Rigid-Body Equations of Motion. Appendix D. Apparent-Mass Effects. Appendix E. Lift of Finite Wings Due to Oscillatory Plunging Acceleration.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
Aerodynamics;Aircraft Structures;Flight Dynamics;Propeller design and performance;Aeronautical history;Fixed wing aircraft;Flying wing aircraft;Design-goal process;Unconventional aircraft;Flying wings;Lighter than air vehicle design;Glide Slope;Lift Coefficient;Lift Curve Slope;Wright Brothers;Trim Condition;Glide Tests;Propulsive Efficiency;Flying Wing;Aerodynamic Center;Pitching Moment Coefficient;Flight Speed;Actuator Disk Theory;Momentum Theory;Symmetrical Airfoil;Mass Center Location;Buckling Load;Thick Airfoil;Aluminum Column;Tapered Wing;Radial Swirl;Double Swept;Aerodynamic Chord;Torsion Box;Outer Portion;Thrust Vector
1. Introduction. 2. Aerodynamic Review. 3. Propeller Analysis. 4. Flying Wing (or Tailless Airplanes). 5. Canard Airplanes and Biplanes. 6. Flight Dynamics. 7. Performance. 8. Balloons and Airships. Appendix A. Multhropp Body-Moment Equation. Appendix B. Alternative Swept-Wing Analysis. Appendix C. Rigid-Body Equations of Motion. Appendix D. Apparent-Mass Effects. Appendix E. Lift of Finite Wings Due to Oscillatory Plunging Acceleration.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
Aerodynamics;Aircraft Structures;Flight Dynamics;Propeller design and performance;Aeronautical history;Fixed wing aircraft;Flying wing aircraft;Design-goal process;Unconventional aircraft;Flying wings;Lighter than air vehicle design;Glide Slope;Lift Coefficient;Lift Curve Slope;Wright Brothers;Trim Condition;Glide Tests;Propulsive Efficiency;Flying Wing;Aerodynamic Center;Pitching Moment Coefficient;Flight Speed;Actuator Disk Theory;Momentum Theory;Symmetrical Airfoil;Mass Center Location;Buckling Load;Thick Airfoil;Aluminum Column;Tapered Wing;Radial Swirl;Double Swept;Aerodynamic Chord;Torsion Box;Outer Portion;Thrust Vector
