Publication Date:
2019-06-27
Description:
The predicted upper and lower bounds power spectra for all of the cases and response items given in Volume 1 are plotted. The flight test power spectra are shown on each prediction plot for the nominal value of angle of attack that most closely agrees with the flexible angle for the prediction. The flight test and prediction conditions are given in tabular form for all cases considered.
Keywords:
AERODYNAMICS
Type:
NASA-CR-3036
Format:
application/pdf