Blade Element Momentum Theory
Blade element momentum theory (BEM) is a fundamental method for analyzing rotor performance by combining blade element aerodynamics with momentum conservation. Developed initially by Froude and refined by Glauert and Leishman, BEM decomposes a rotor into radial blade elements, computes local aerodynamic forces, and sums contributions to predict total thrust, torque, power, and efficiency. BEM is standard for helicopter, wind turbine, and propeller design.
Allikakirje
Tsiteeringud kopeeritud meetodi allikakirjest sõna-sõnalt. Nendest ei saa järeldada väidete tasemel kinnitust.
- Froude, W. (1889). On the elementary relation between pitch, slip, and propulsive efficiency. Transactions of the Institution of Naval Architects, 30, 94–103. · URL
- Glauert, H. (1935). The Elements of Aerofoil and Airscrew Theory. Cambridge University Press. · URL
- Leishman, J. G. (2006). Principles of Helicopter Aerodynamics (2nd ed.). Cambridge University Press. · URL
Kureeritud väited
Väited on salvestatud tõendite registrisse, igal oma hinnanguga.
See vaade ei loo väite hinnangut, kui registris seda pole.
Seotud meetodid
Genereeritud meetodigraafist ja kuvatud masina soovitatud seostena – väiteid ei järeldata.