Что такое findslide.org?

FindSlide.org - это сайт презентаций, докладов, шаблонов в формате PowerPoint.


Для правообладателей

Обратная связь

Email: Нажмите что бы посмотреть 

Яндекс.Метрика

Презентация на тему The Aerodynamics Of A Single-Blade Rotor

Why did we start our investigation?Because of curiosity;The interest to the super light aircraft;To evaluate the correspondence of obtained results to the real winged seed flight parameters.
The Aerodynamics Of A Single-Blade RotorThe Mathematical Model Of Single-Blade Rotor FlightPerformed Why did we start our investigation?Because of curiosity;The interest to the super The Aim of the workTo investigate the aerodynamics of single blade rotor We assumed the model of a winged seed aerodynamics and, based on The previous researches that met this topic had created the different models of SBR Gluhareff MEG-1x MEG-1XMEG-1X was created by American engineer Eugene Gluhareff in 1955. The creator In USSR the pioneer in creation of single bladed helicopter was the AliSportNowadays the only firm, Alisport, creates the full-size aircraft with single blade Mathematical Model dT=(dL·cosβ*- dD·sinβ*)·cosβ* dQ= - dL·sinβ* - dD·cosβ*dM=dQ· r · cosβdL=CL(α) · ρ dML = dL·rdMCfb= dFcfb·r·sinβdFcfb = dmb ·ωz*2·r·cosβ = MB/(R-rh)dMWB= dmb·g·r·cosβdMCfRD= dmRD ·ωz*2·r·cosβMCFW = 1/2mw·ωz *2·rh2·sin2βMW= mw·g·rh·cosβ Thank You for attentionПоліт, 2012
Слайды презентации

Слайд 2 Why did we start our investigation?
Because of curiosity;
The

Why did we start our investigation?Because of curiosity;The interest to the

interest to the super light aircraft;
To evaluate the correspondence

of obtained results to the real winged seed flight parameters.

Слайд 3 The Aim of the work
To investigate the aerodynamics

The Aim of the workTo investigate the aerodynamics of single blade

of single blade rotor (SBR);
To construct its (SBR)

mathematical model;
To get acquainted with results of scientific researches in this area;
To solve the equation of motion of SBR: to find the angular velocity of autorotation.
To sophisticate the idea of SBR motion.


Слайд 4 We assumed the model of a winged seed

We assumed the model of a winged seed aerodynamics and, based

aerodynamics and, based on it, we decided to create

the single blade rotor.


Слайд 5 The previous researches that met this topic had

The previous researches that met this topic had created the different models of SBR

created the different models of SBR


Слайд 6 Gluhareff MEG-1x

Gluhareff MEG-1x

Слайд 7 MEG-1X
MEG-1X was created by American engineer Eugene Gluhareff

MEG-1XMEG-1X was created by American engineer Eugene Gluhareff in 1955. The

in 1955. The creator of MEG-1X, following the ancient

wisdom “the less, the better”, has coherently thrown out all the excessive details, he did not spare even the blades: only one of them stayed with a jet engine, attached to its end.

Слайд 8 In USSR the pioneer in creation of single

In USSR the pioneer in creation of single bladed helicopter was

bladed helicopter was the student of Kharkov Aviation Institute,

Yuri Marinchenko. The original version of helicopter was planned as a backpack weighting 30 kg. He developed this idea during a year and, in 1971 the model was established.



Слайд 9 AliSport
Nowadays the only firm, Alisport, creates the full-size

AliSportNowadays the only firm, Alisport, creates the full-size aircraft with single

aircraft with single blade rotor.
They created the famous

one-bladed gliders.

Слайд 10 Mathematical Model

Mathematical Model

Слайд 12
dT=(dL·cosβ*- dD·sinβ*)·cosβ*
dQ= - dL·sinβ* - dD·cosβ*
dM=dQ· r

dT=(dL·cosβ*- dD·sinβ*)·cosβ* dQ= - dL·sinβ* - dD·cosβ*dM=dQ· r · cosβdL=CL(α) ·

· cosβ
dL=CL(α) · ρ W2·c(r)dr
dD=CD(α) · ρ W2·c(r)dr

W2=U2+ Vz*2
U=ωz2

·r· cosβ

α=φ(r) - β*

β*=arctan Vz*÷U




Слайд 13 dML = dL·r

dMCfb= dFcfb·r·sinβ
dFcfb = dmb ·ωz*2·r·cosβ

=

dML = dL·rdMCfb= dFcfb·r·sinβdFcfb = dmb ·ωz*2·r·cosβ = MB/(R-rh)dMWB= dmb·g·r·cosβdMCfRD= dmRD ·ωz*2·r·cosβMCFW = 1/2mw·ωz *2·rh2·sin2βMW= mw·g·rh·cosβ

MB/(R-rh)


dMWB= dmb·g·r·cosβ


dMCfRD= dmRD ·ωz*2·r·cosβ
MCFW = 1/2mw·ωz *2·rh2·sin2β
MW= mw·g·rh·cosβ


  • Имя файла: the-aerodynamics-of-a-single-blade-rotor.pptx
  • Количество просмотров: 94
  • Количество скачиваний: 0