Flight performance of aircraft

Bibliographic Information

Flight performance of aircraft

by S.K. Ojha

(AIAA education series)

American Institute of Aeronautics and Astronautics, c1995

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Note

Includes bibliographical references and index

Description and Table of Contents

Description

This text describes the basic forces which dictate and decide the performance of an aircraft. It is aimed at pilots and flight-test engineers seeking answers to questions of flight mechanics. Referring to real-life situations, performance analysis is presented for most phases of flying, including takeoff, climb, cruise, turn, descent and landing. To improve confidence in dealing with these situations, a list of problems is provided at the end of each chapter to encourage trouble-shooting and theory comprehension. Charts, figures and references reinforce and complement the text throughout.

Table of Contents

  • Aircraft, Basic Forces, and Performance
  • Atmosphere and Flying Weather
  • Aerodynamic Forces on Aircraft
  • Propulsive Thrust by Jet Engine
  • Propulsive Power by Piston-Prop Engine
  • Altitudes, Airspeeds, and Wind Speeds
  • Gliding and Unpowered Flights
  • Cruising Flights of Turbojet Aircraft
  • Optimizations of Cruising Flights of Turbojet Aircraft
  • Climbing Flights of Turbojet Aircraft
  • Turning Flights of Turbojet Aircraft
  • Cruising Flights of Piston-Prop Aircraft
  • Climbing Flights of Piston-Prop Aircraft
  • Co-ordinated Turning Flights of Piston-Prop Aircraft
  • Takeoff and Landing Performance
  • Aerobatic Maneouvres and Flight Boundaries
  • Performance Evaluation by Test Flights
  • Weather Hazards and Flying
  • Weather Observations, Reports, and Forecasts to Flying.

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Details
  • NCID
    BA28022863
  • ISBN
    • 1563471132
  • LCCN
    95004456
  • Country Code
    us
  • Title Language Code
    eng
  • Text Language Code
    eng
  • Place of Publication
    Washington, DC
  • Pages/Volumes
    516 p.
  • Size
    24 cm
  • Classification
  • Subject Headings
  • Parent Bibliography ID
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