An evaluation of current prediction methodologies to estimate the aerodynamic uncertainties identified for the E205 configuration is presented. This evaluation was accomplished by comparing predicted and wind tunnel test data in three major categories: untrimmed longitudinal aerodynamics; trimmed longitudinal aerodynamics; and lateral-directional aerodynamic characteristics.
Analysis of Wind Tunnel Test Results for a 9.39-Per Cent Scale Model of a Vstol Fighter/Attack Aircraft. Volume 2: Evaluation of Prediction Methodologies
1980
139 pages
Report
Keine Angabe
Englisch