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aerodynamic balance airfoil altitude angle of attack angle of yaw annulus average balanced elevator blunt nose blunt-nose brake horsepower characteristics chord control surface cowling curves cylinder density altitude downwash drag drag coefficient dynamic pressure effect elevat or deflection elevator deflections engine Figure flap deflections flaps retracted flight function of angle fuselage fuselage-tail hinge-moment coefficient horizontal tail surface impact Increments of lift inst Langley Langley Field lift and elevator lift coefficient measured NACA Fig Nacelles º º ºov plain elevator plain flap propeller sealed gap sharp-nose slip stream span spect ratio stall surveys t e st tab deflection tack tail plane temperature throughout the yaw tile tion tube unsealed unst wind tunnel wing XP-42 airplane yaw range zero Zºº