flight school; Dictionary_of_Aviation
Dictionary of
Aviation
second edition
Originally published by Peter Collin Publishing
as Dictionary of Aeronautical English
First edition published 1999
Second edition published 2005 by Bloomsbury Publishing
Plc
Reprinted 2007 by
_&C Black Publishers Ltd
38 Soho Square, London W1D 3HB
Copyright © David Crocker and Peter Collin Publishing
Ltd. 1999
Revisions and additional material © A&C Black
Publishers Ltd 2007
All rights reserved. No part of this publication may
be reproduced in any form or by any means without the
prior written permission of the publishers.
A CIP record for this book is available from the
British Library
eISBN-13: 978-1-4081-0226-8
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Dictionary_of_Aviation,
flight school :WEIGHTAND BALANCE AND AIRPLANE
WEIGHTAND BALANCE AND AIRPLANE
INTRODUCTION
Airplane performance is the capability of the
airplane, if operated within its limitations, to accomplish maneuvers which
serve a
specific purpose. For example, most present-day
airplanes are designed clean and sleek, which results in greater range, speed,
payload, and increased efficiency. This type of
airplane is preferred for cross-country flights. Airplanes used for short
flights and
carrying heavy loads, such as those used in certain
agricultural operations, are designed differently, but still exhibit good
performance for their purpose. Some of the factors
which represent good performance are short takeoff and landing distance,
increased
climb capability, and greater speeds using less fuel.
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WEIGHT AND BALANCE,
flight school:Aircraft Performance
Introduction
This chapter discusses the factors that affect aircraft
performance, which include the aircraft weight, atmospheric
conditions, runway environment, and the fundamental
physical laws governing the forces acting on an aircraft.
Importance of Performance Data
The performance or operational information section of the
Aircraft Flight Manual/Pilot’s Operating Handbook (AFM/
POH) contains the operating data for the aircraft; that is, the
data pertaining to takeoff, climb, range, endurance, descent,
and landing. The use of this data in flying operations is
mandatory for safe and efficient operation. Considerable
knowledge and familiarity of the aircraft can be gained
through study of this material.
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flight schoole:aerodynamics of flight
aerodynamics of flight
Forces Acting on the Aircraft
Thrust, drag, lift, and
weight are forces that act upon all aircraft in flight. Understanding how these
forces work and knowing how to control them with the use of power and flight
controls are essential to flight. This chapter discusses the aerodynamics of
flight—how design, weight, load factors, and gravity affect an aircraft during
flight maneuvers.
The four forces acting on
an aircraft in straight-and-level, unaccelerated flight are thrust, drag, lift,
and weight. They
are defined as follows:
• Thrust—the forward force
produced by the powerplant/ propeller or rotor. It opposes or overcomes the
force of drag. As a general rule, it acts parallel to the longitudinal axis.
However, this is not always the case, as explained later.
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flight school: Principles of Flight
Principles of Flight
Aerospace Series List
Cooperative Path
Planning of Unmanned Aerial
Vehicles
Tsourdos et al
November 2010
Principles of Flight
for Pilots Swatton October 2010
Air Travel and
Health: A Systems Perspective Seabridge et al September 2010
Design and Analysis
of Composite Structures:
With Applications to
Aerospace Structures
Kassapoglou September
2010
Unmanned Aircraft
Systems: UAVS Design,
Development and
Deployment
Austin April 2010
Introduction to
Antenna Placement &
Installations
Macnamara April 2010
Principles of Flight
Simulation Allerton October 2009
Aircraft Fuel Systems
Langton et al May 2009
The Global Airline
Industry Belobaba April 2009
Computational
Modelling and Simulation of
Aircraft and the
Environment: Volume 1 –
Platform Kinematics
and Synthetic
Environment
Diston April 2009
Handbook of Space
Technology Ley, Wittmann Hallmann April 2009
Aircraft Performance
Theory and Practice for
Pilots
Swatton August 2008
Surrogate Modelling
in Engineering Design: A
Practical Guide
Forrester, Sobester,
Keane August 2008
Aircraft Systems, 3rd Edition Moir & Seabridge March 2008
Introduction to
Aircraft Aeroelasticity And
Loads
Wright & Cooper
December 2007
Stability and Control
of Aircraft Systems Langton September 2006
Military Avionics
Systems Moir & Seabridge February 2006
Design and
Development of Aircraft Systems Moir & Seabridge June 2004
Aircraft Loading and
Structural Layout Howe May 2004
Aircraft Display
Systems Jukes December 2003
Civil
Avionics Systems
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Aviation Courses: air law
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