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Archive / Aerodynamics for Naval Aviators / Aerodynamics for Naval Aviators: Chapter 5

Chapter 5

Chapter 5

NAVAIR 00-80T-80 (1965)

NAVWEPS OO-BOT-80

TABLE OF CONTENTS

CHAPTER 5. OPERAilNG STRENGTH LIMITATIONS

GENERAL OEFlNlTlONS AND STRUCTURAL REQUlREMENTS

STATIC STRENGTH .._.......... ~.~~~.~ ~..~

Limit load

Factor of safety

Material properties

SERVICE LIFE

Pati

Loa r

e consideration

spectrum attd cumulative damage

Creep considerations

AEROELASTIC EFFECTS.

Stiffness and rigidity

AIRCRAFT LOADS AND OPERATING LIMITATIONS

FLIGHT LOADS-MANEUVERS AND GUSTS.

Loadfactor.....................................................

Maneuvering load factors.. .I

Maximum lift capability

Effect of gross weight

^ . ._ ClllStlOadtacfors..............,.................................

Gust load increment

Effect of gust intensity and lift curve slope

Effect of wing loading and altitude

Effect of overstrea.

THE V-n OR V-g DIAGRAM.

Effect of weight, configuration;altihtde, and symmetry of Ior-Ang

Limit load factors

Ultitnute load facvxs

Maximum lift capability

Limit airspeed

Operating env+pe

Maneuver’speed and penetration of turbulence

EFFECT OF HIGH SPEED FLIGHT..

Critical gust

Aileron reversal

Divergence

PIutter

Compressibility problems

LANDING AND GROUND LOADS.

Landing load factor

Effect of touchdown rate of descent

Effect of gross weight

Ported landing on unprepared .surfaces

EFFECT OF OVERSTRESS ON SERVICE

Recognition of overstress’damage

Importance of operating limitations

LIFE

,...

,..,

,’ 334

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