4 pages matching drag coefficient in this book
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additional rockets aero Aerodynamic Centre aircraft angle for different angle of incidence bearing centres body calculated Calibration chord complete model computing sheet constant corr decreases Diagram diameter High Speed downwash angle drag coefficient Dynamic Pressure formula front struts fuselage axis headings on computing high Mach Numbers incidence range incompressible low increased by 0.5 Kach lift curve slope lift gradient lift Pig longitudinal stability low speeds Mach Number range Maoh Mcorr methods of evaluation model without tailplane Natter negative incidences normal ohord Pitching moment correction positive elevator angles Prandtl rule protocol reproduced graphically shield and sting shown in Fig speed tunnel static pressure strut corrections strut in shield supporting rig tail strut teats tests total head Total model valid for high Variation of elevator wake whole rig wind shield wind tunnel zero lift