IHS ESDU Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers. 72024

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ESDU 72024 provides a means of estimating the lift-curve slope at zero lift, zero-lift incidence, zero-lift pitching moment coefficient and chordwise location of the aerodynamic centre for any aerofoil in compressible inviscid airflow from a knowledge of a number of parameters characterising the thickness distribution and camber line shape. The data, which are presented in graphical form, were derived by correlating the results of a large number of calculations obtained from exact theory.
Description
ESDU 72024 provides a means of estimating the lift-curve slope at zero lift, zero-lift incidence, zero-lift pitching moment coefficient and chordwise location of the aerodynamic centre for any aerofoil in compressible inviscid airflow from a knowledge of a number of parameters characterising the thickness distribution and camber line shape. The data, which are presented in graphical form, were derived by correlating the results of a large number of calculations obtained from exact theory.

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Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers. - 72024 - IHS ESDU
London, United Kingdom
Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers.
72024
Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers. 72024
ESDU 72024 provides a means of estimating the lift-curve slope at zero lift, zero-lift incidence, zero-lift pitching moment coefficient and chordwise location of the aerodynamic centre for any aerofoil in compressible inviscid airflow from a knowledge of a number of parameters characterising the thickness distribution and camber line shape. The data, which are presented in graphical form, were derived by correlating the results of a large number of calculations obtained from exact theory.

ESDU 72024 provides a means of estimating the lift-curve slope at zero lift, zero-lift incidence, zero-lift pitching moment coefficient and chordwise location of the aerodynamic centre for any aerofoil in compressible inviscid airflow from a knowledge of a number of parameters characterising the thickness distribution and camber line shape. The data, which are presented in graphical form, were derived by correlating the results of a large number of calculations obtained from exact theory.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 72024
Product Name Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers.
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