Some Procedures for Use in Performance Prediction of Proposed Aircraft Designs Bureau of Naval Weapons, Dept. of the Navy

Format:

Conference/Event

Author/Creator:

Linden, J. E., author.

Conference Name:

Aeronautic and Space Engineering and Manufacturing Meeting (1965-10-04 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

An empirical method for predicting subsonic minimum drag, drag-due-to-lift, and subsonic drag rise of proposed jet aircraft designs is presented. The method is designed for use in the absence of wind tunnel test data on a model of the specific configuration of interest. Estimates, based on this method, have correlated well with flight test results

Notes:

Vendor supplied data

Publisher Number:

650800

Access Restriction:

Restricted for use by site license