Effects of Symmetric and Asymmetric Thrust Reversal on the Aerodynamic Characteristics of a Model of a Twin-engine Airplane
This NASA technical report from 1953, produced by the National Advisory Committee for Aeronautics, documents wind-tunnel tests of a model twin-engine airplane with symmetric and asymmetric thrust reversal, written for aeronautical engineers and researchers. Its pictures are dense grey-ruled graph plots of coefficients against angle of attack and control deflection, with labelled curves and small data points, offering a designer little beyond a sparse engineering-chart aesthetic of fine grids and thin black lines.
