The model showed acceptable correlation and was used to conduct a thorough parametric study on various design configurations.
In this sense, it was verified that the adjustment indicators with three response options (second model) presented a good fit (χ2/df = 1.56, TLI = 0.94, CFI = 0.95, RMSEA = 0.04) and the model with five response options (first model) showed acceptable but poor fit (χ2/df = 2.92, TLI = 0.87, CFI = 0.89, RMSEA = 0.07) (Table 1) (Marôco, 2014).
As the P.1127 had been developed at a time of deep UK defense cuts, Hawker had to seek commercial funding, and significant engine development funding came from the U.S. Wind tunnel tests conducted by NASA Langley Research Center using a sub-scale model showed acceptable flight characteristics.
This model showed acceptable model fit with a chi square value of 364.41 df = 512).
In the current study, this single-factor model showed acceptable fit, supporting the validity of using the total score.
The constrained model showed acceptable model fit: RMSEA = 0.073 900% CI = 0.071, 0.074), CFI = 0.953 (see table 2 for the other fit indices).
The constrained model showed acceptable model fit, RMSEA = 0.062 (90% CI = 0.061, 0.064), CFI = 0.972 (other fit indices are reported in table 2).
The prediction model showed acceptable discrimination (AUC >0.70 but <0.80), a good goodness-of-fit (HL test, P = 0.50) and had a shrinkage factor of 0.83.
The gamma and Pearson models showed acceptable performances in simulating both limbs of the unit hydrographs.
All models show acceptable fits with RMSEA values ranging from.044 to.054, CFI values ranging from.906 to.938 and TLI values ranging from.902 to.920.
