Suggested values for L/D, Cj, <math xmlns='http://www.w3.org/1998/Math/MathML'> <mrow> <msub> <mi>η</mi> <mi>P</mi> </msub> </mrow> </math>, Cp and for several mission phases.

Table 4: Suggested values for L/D, C_j, $η_{P}$ , C_p and for several mission phases.


Single engine airplane	8-10	0.5-0.7	0.8