DETERMINATION OF ICE SHAPES AND THEIR EFFECT ON THE AERODYNAMIC CHARACTERISTICS FOR THE UNPROTECTED TAIL OF THE A 300.

Boris Laschka; Rudolf E. Jesse

DETERMINATION OF ICE SHAPES AND THEIR EFFECT ON THE AERODYNAMIC CHARACTERISTICS FOR THE UNPROTECTED TAIL OF THE A 300.

Boris Laschka, Rudolf E. Jesse

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1 Scopus citations

Abstract

The tail surfaces of the European Airbus A 300 are not equipped with a de-icing or anti-icing system. It could be shown by analysis and tests that, under maximum icing conditions defined in FAR 25, the aircraft remains completely safe, stable and controllable within its flight envelope. This paper outlines the procedure applied to determine the ice accretion on the unprotected surfaces and its influence on the aerodynamic characteristics of the airplane.

Original language	English
Pages	409-418
Number of pages	10
State	Published - 1974

Cite this

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title = "DETERMINATION OF ICE SHAPES AND THEIR EFFECT ON THE AERODYNAMIC CHARACTERISTICS FOR THE UNPROTECTED TAIL OF THE A 300.",

abstract = "The tail surfaces of the European Airbus A 300 are not equipped with a de-icing or anti-icing system. It could be shown by analysis and tests that, under maximum icing conditions defined in FAR 25, the aircraft remains completely safe, stable and controllable within its flight envelope. This paper outlines the procedure applied to determine the ice accretion on the unprotected surfaces and its influence on the aerodynamic characteristics of the airplane.",

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year = "1974",

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AU - Jesse, Rudolf E.

PY - 1974

Y1 - 1974

N2 - The tail surfaces of the European Airbus A 300 are not equipped with a de-icing or anti-icing system. It could be shown by analysis and tests that, under maximum icing conditions defined in FAR 25, the aircraft remains completely safe, stable and controllable within its flight envelope. This paper outlines the procedure applied to determine the ice accretion on the unprotected surfaces and its influence on the aerodynamic characteristics of the airplane.

AB - The tail surfaces of the European Airbus A 300 are not equipped with a de-icing or anti-icing system. It could be shown by analysis and tests that, under maximum icing conditions defined in FAR 25, the aircraft remains completely safe, stable and controllable within its flight envelope. This paper outlines the procedure applied to determine the ice accretion on the unprotected surfaces and its influence on the aerodynamic characteristics of the airplane.

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EP - 418

ER -

DETERMINATION OF ICE SHAPES AND THEIR EFFECT ON THE AERODYNAMIC CHARACTERISTICS FOR THE UNPROTECTED TAIL OF THE A 300.

Abstract

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