New Method of Determining the Polar Curve of an Airplane in Flight PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download New Method of Determining the Polar Curve of an Airplane in Flight PDF full book. Access full book title New Method of Determining the Polar Curve of an Airplane in Flight by B. N. Yegorov. Download full books in PDF and EPUB format.
Author: B. N. Yegorov Publisher: ISBN: Category : Aerofoils Languages : en Pages : 688
Book Description
A fundamental defect of existing methods for the determination of the polar of an airplane in flight is the impossibility of obtaining the thrust or the resistance of the propeller for any type airplane with any type engine. The new method is based on the premise that for zero propeller thrust the mean angle of attack of the blade is approximately the same for all propellers if this angle is reckoned from the aerodynamic chord of the profile section. This angle was determined from flight tests. Knowing the mean angle of the blade setting the angle of attack of the propeller blade at zero thrust can be found and the propeller speed in gliding obtained. The experimental check of the new method carried out on several airplanes gave positive results. The basic assumptions for the construction of the polars and the method of analyzing the flight data are given.
Author: B. N. Yegorov Publisher: ISBN: Category : Aerofoils Languages : en Pages : 688
Book Description
A fundamental defect of existing methods for the determination of the polar of an airplane in flight is the impossibility of obtaining the thrust or the resistance of the propeller for any type airplane with any type engine. The new method is based on the premise that for zero propeller thrust the mean angle of attack of the blade is approximately the same for all propellers if this angle is reckoned from the aerodynamic chord of the profile section. This angle was determined from flight tests. Knowing the mean angle of the blade setting the angle of attack of the propeller blade at zero thrust can be found and the propeller speed in gliding obtained. The experimental check of the new method carried out on several airplanes gave positive results. The basic assumptions for the construction of the polars and the method of analyzing the flight data are given.
Author: B. N. Yegorov
Author: B. N. Yegorov
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: Earth Resources Laboratory (U.S.)