Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests: Thesis (Classic Reprint) - Hardcover

James Sargent Russell

 
9780265575178: Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests: Thesis (Classic Reprint)

Synopsis

Propeller characteristics and slipstream effects come to life through wind-tunnel tests on a high-wing monoplane model.

This study examines how propeller power, blade setup, and slipstream influence lift, drag, and stability. It translates complex measurements into practical insights for airplane performance.

The authors explore how model data, scale considerations, and wind-tunnel factors affect results, and they show how power on and power off conditions change the airplane’s behavior. You’ll see how thrust, drag, and pitching moments are measured and interpreted, and how efficiency is evaluated through dimensionless coefficients and performance relations. The work also discusses how tail effects and downwash factor into overall stability.
  • How power input and propeller configuration alter lift, drag, and pitching moment
  • How model tests relate to full-scale expectations and the role of Reynolds number and scale effects
  • Methods for calculating thrust, torque, velocity, and propulsive efficiency
  • Insights into tail influence and slipstream on longitudinal stability
Ideal for readers of aeronautical engineering and graduate studies, this edition offers a detailed look at wind-tunnel methodology and the practical interpretation of propulsion and stability data.

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