Reduction of Pressure Survey Data with Regression Analysis

Format:

Conference/Event

Author/Creator:

Yost, J. D. (James D.), author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1976-04-06 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1976

Summary:

A new method has been developed for using regression analysis to obtain equations for aircraft pressure coefficients. This method allows wind tunnel or flight test pressure survey data to be collected at a lower cost with accurate coverage of non-linear mach effects. An equation for a given structural location includes mach effects and all other significant independent variables for their full aircraft operational range. Many test conditions are reduced to a few composite variable coefficients which may easily be used for further aircraft design conditions for strength or fatigue

Notes:

Vendor supplied data

Publisher Number:

760451

Access Restriction:

Restricted for use by site license