... Glide" Climbing Flight Gliding, Climbing, and Turning Flight Performance Robert Stengel, Aircraft Flight Dynamics, MAE 331, 2012 ! Copyright 2012 by Robert Stengel. All rights reserved. For educational ... Flight Envelope Flight Envelope Determined by Available Thrust" • Flight ceiling defined by available climb rate" – Absolute: 0 ft/min"...
Ngày tải lên: 04/07/2014, 19:25
... ∂ ψ ∂ψ " # $ $ $ $ $ $ $ % & ' ' ' ' ' ' ' • Four (6 x 6) blocks distinguish longitudinal and lateral-directional effects " F = F Lon F Lat−Dir Lon F Lon Lat−Dir F Lat−Dir " # $ $ % & ' ' Effects of longitudinal ... Spring" Spring Force vs. Displacement" Spring" Damper" Displacement"...
Ngày tải lên: 04/07/2014, 19:25
Aircraft Flight Dynamics Robert F. Stengel Lecture15 Transfer Functions and Frequency Response
... } Δu(s) Transfer Function Matrix" • Frequency-domain effect of all inputs on all outputs" • Assume control effects do not appear directly in the output: H u = 0" • Transfer function ... = h 11 h 12 h 21 h 22 ! " # # $ % & & adj s − f 11 ( ) − f 12 − f 21 s − f 22 ! " # # $ % & & det s − f 11 ( ) − f 12 − f 21 s − f 22 ( ) ( ) * *...
Ngày tải lên: 04/07/2014, 19:27
Aircraft Flight Dynamics Robert F. Stengel Lecture1 Introduction to Flight Dynamics
... History ! Aerodynamics of Airplane Configurations ! Cruising Flight Performance ! Gliding, Climbing, and Turning Performance ! Nonlinear, 6-DOF Equations of Motion ! Linearized Equations of Motion ! ... only.! http://www.princeton.edu/ ~stengel/ MAE331.html! ! Dynamics & Control of Atmospheric Flight ! Configuration Aerodynamics ! Aircraft Performance ! ...
Ngày tải lên: 04/07/2014, 19:19
Aircraft Flight Dynamics Robert F. Stengel Lecture2 PointMass Dynamics and Aerodynamic Thrust Forces
... Frame" C X C Y C Z ⎡ ⎣ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ B = axial force coefficient side force coefficient normal force coefficient ⎡ ⎣ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ C D C Y C L ⎡ ⎣ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ = drag coefficient side force coefficient lift coefficient ⎡ ⎣ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ • ... = v x v y v z ⎡ ⎣ ⎢ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ ⎥ F I = f x f y f z ⎡ ⎣ ⎢ ⎢ ⎢ ⎢ ⎤ ⎦ ⎥ ⎥ ⎥ ⎥ I = F gravity + F aerodynamics + F thrust ⎡...
Ngày tải lên: 04/07/2014, 19:20
Aircraft Flight Dynamics Robert F. Stengel Lecture3 Aviation History Mythology to 1990
... effects" • Short-Takeoff -and- Landing (STOL) aircraft augment takeoff/landing lift in many ways, e.g.," – Full-span flaps" – Deflected thrust" Grumman F8 F! Grumman F4 F! GB R1! C T o ,C T V ,C T δ T ,C L δ T World ... compressibility effects on drag! • Dramatic change in stability, control, and flying qualities! • North American FJ-1 and FJ-4 Fury! • Republic...
Ngày tải lên: 04/07/2014, 19:21
Aircraft Flight Dynamics Robert F. Stengel Lecture5 Configuration Aerodynamics 2.
... Axes" f B = X B Y B Z B ! " # # # $ % & & & m B = L B M B N B ! " # # # $ % & & & Force Vector" Moment Vector" r × f = i j k x y z f x f y f z = yf z − zf y ( ) i + zf x − xf z ( ) j + xf y − yf x ( ) k m = yf z − zf y ( ) zf x − xf z ( ) xf y − yf x ( ) # $ % % % % & ' ( ( ( ( = rf ... Dihedral effect" • Vertical t...
Ngày tải lên: 04/07/2014, 19:22
Aircraft Flight Dynamics Robert F. Stengel Lecture6 Cruising Flight Performance
... Cruising Flight Performance Robert Stengel, Aircraft Flight Dynamics, MAE 331, 2012! Copyright 2012 by Robert Stengel. All rights reserved. For educational use only.! http://www.princeton.edu/ ~stengel/ MAE331.html! http://www.princeton.edu/ ~stengel/ FlightDynamics.html! • ... 0 • Satisfy necessary condition for a maximum" • Lift-to-drag ratio" • Lift coefficient...
Ngày tải lên: 04/07/2014, 19:24
Aircraft Flight Dynamics Robert F. Stengel Lecture8 Aircraft Equations of Motion 1
... theorem" • Model in Pro/ENGINEER, etc." Aircraft Equations of Motion - 1 Robert Stengel, Aircraft Flight Dynamics, MAE 331, 2012 " • 6 degrees of freedom" • Angular kinematics" • ... geometric shapes with uniform density" Moments and Products of Inertia" (Bedford & Fowler)" • Construct aircraft moments and products of...
Ngày tải lên: 04/07/2014, 19:25