ESDU TM 178
ESDU TECHNICAL MEMORANDUM
Effect of wing-mounted engine nacelles of propeller-driven aircraft on lateral stability derivatives in sideslip
Abstract:
Available as part of the ESDU Series on Aerodynamics. For information on all ESDU validated engineering data please contact us using the details on the preceding page.
This Memorandum gives a tentative method for predicting (Yv )n , (Nv )n and(Lv )n , the effects of wing-mounted engine nacelles of propeller-driven aircraft on lateral stability derivatives in sideslip.
Indexed under:
- Derivatives
- Nacelle
- Rolling Moment Due To Sideslip (Lv or Cl β)
- Sideforce Due To Sideslip (Yv or Cy β)
- Yawing Moment Due To Sideslip (Nv or Cnβ)
Details:
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