Aerodynamics, Aeronautics and Flight MechanicsA single, comprehensive, in-depth treatment of both basic, and applied modern aerodynamics. Covers the fluid mechanics and aerodynamics of incompressible and compressible flows, with particular attention to the prediction of lift and drag characteristics of airfoils and wings and complete airplane configurations. Following an introduction to propellers, piston engines, and turbojet engines, methods are presented for analyzing the performance of an airplane throughout its operating regime. Also covers static and dynamic longitudinal and lateral-directional stability and control. Includes lift, drag, propulsion and stability and control data, numerical methods, and working graphs. |
From inside the book
Results 1-3 of 87
Page 203
... Reference 4.10 . In this case , the airplane is the Gates Learjet Model 25 pictured in Figure 4.27 . Table 4.5 was prepared on the basis of Reference 4.10 . The authors of the reference chose to base Ca for each item on the wing area ...
... Reference 4.10 . In this case , the airplane is the Gates Learjet Model 25 pictured in Figure 4.27 . Table 4.5 was prepared on the basis of Reference 4.10 . The authors of the reference chose to base Ca for each item on the wing area ...
Page 554
... Reference 8.2 that the time derivative of a vector defined in a rotating reference frame is given by dA SA = dt δι + wXA ( 9.4 ) SA / St is the apparent derivative as viewed in the moving reference system . w is the angular velocity ...
... Reference 8.2 that the time derivative of a vector defined in a rotating reference frame is given by dA SA = dt δι + wXA ( 9.4 ) SA / St is the apparent derivative as viewed in the moving reference system . w is the angular velocity ...
Page 619
... reference . The scatter and overlapping of the points in Reference 10.1 appear to rule out any valid definition of the criteria as a function of μ . Instead , the graph of Figure 10.9 is offered as representative of any μ value . In the ...
... reference . The scatter and overlapping of the points in Reference 10.1 appear to rule out any valid definition of the criteria as a function of μ . Instead , the graph of Figure 10.9 is offered as representative of any μ value . In the ...
Contents
ONE INTRODUCTION 119 | 1 |
TWO FLUID MECHANICS | 16 |
THREE THE GENERATION OF LIFT | 61 |
Copyright | |
11 other sections not shown
Common terms and phrases
aerodynamic center aileron aircraft airplane altitude angle of attack approximately aspect ratio blade boundary layer C₁ calculated camber center of gravity Cherokee 180 chord climb component compressor configuration constant cruise deflected delta wing distance drag coefficient effect engine equal Equation estimated flight flow fluid force form drag free-stream ft² fuel function fuselage given horizontal tail increase increment induced drag interference drag laminar leading edge lift coefficient lift curve lift line Mach number maximum NACA normal parasite drag pictured in Figure planform presented in Figure propeller Reference Reynolds number roll sea level shock wave shown in Figure skin friction slug-ft² speed stability stall static pressure subsonic supersonic surface takeoff temperature thickness thrust trailing edge trim true airspeed turbine turbofan turbojet V₁ velocity vertical tail vortex weight winglet yawing zero lift