Fizik Ödev Yardımı

Fizik, tüm doğa bilimleri arasında çok önemli bir konudur, yaşamın harikalarını açıklamak için kullanılır ve aynı zamanda çalışılması en zor konulardan biridir.

QuestionAI, etkileşim halindeki kuvvetler altındaki moleküllerin eşlik eden yörüngeleri ile her bir atom ve onun özellikleri hakkında bilgi edinebileceğiniz, fiziğe yeni başlayanlar için zengin ve kolay bir fizik problemi çözücüdür. Elbette galaksiler arasında saklı sırları diğer fizik meraklılarıyla da keşfedebilirsiniz. Tahminlerinizi ve sorularınızı yapay zekaya cesurca yöneltin; kolayca güvenilir yanıtlar bulacaksınız.

Question 3 (10+10=20 Point): A symmetric airfoil operates at a small angle of attack (alpha =2^circ ) in subsonic flow. The lift coefficient is given by C_(L)=2pi alpha (with alpha in radians). (a) Calculate the lift coefficient (C_(L)) (b) If the chord length is 1.5 m, wing span is 2 m and the airspeed is 30m/s,rho _(infty )=1.225kg/m^3 determine the lift force.

Question 4(10+10=20 Point): A symmetric airfoil operates at a small angle of attack (alpha =2^circ ) in subsonic flow. The lift coefficient is given by C_(L)=2pi alpha (with a in radians). (a) Calculate the lift coefficient (C_(L)) (b) If the chord length is 1.5 m, wing span is 2 m and the airspeed is 30m/s,rho _(infty )=1.225kg/m^3 determine the lift force.

8. Yekta elinde bulunan 2 kg kütleli bir topu duvara dogru sabit 10m/s hiz ile firlattiginda top duvardan sabit 5m/s hiz ile geri dônmektedir. Top ile duvarin etkileşim süresi 0,02 saniye oldu guna góre duvarin topa uyguladig ortalama kuwet kaç N dur?(Sürtünmeler onemsiz) A) 300 B) 400 C) 500 D) 1000 E) 1500

Question 4 (10+10=20 Point): A symmetric airfoil operates at a small angle of attack (alpha =2^circ ) in subsonic flow. The lift coefficient is given by C_(L)=2pi alpha (with alpha in radians). (a) Calculate the lift coefficient (C_(L)) (b) If the chord length is 1.5 m.wing span is 2 m and the airspeed is 30m/s,rho _(infty )=1.225kg/m^3 determine the lift force.

1- Consider an aircraft flying due east along the equator. Define an Earth-fixed coordinate system F_(E) at zero longitude and zero latitude, and a local horizontal coordinate system F_(H) fixed to the center-of-gravity (CG) of the aircraft.Describe the relationship between the axes of f FE and F_(E) F_(H) at the instant the aircraft is at zero longitude and zero latitude, and again at the instant it is at 180 deg east longitude and zero latitude. 2 -An airplane is in a spin with constant phi =-50^circ and constant Theta =-50^circ See Figures 4.2 and 4.3 in your textbook. The rotation rate is constant as well, psi =30deg/s . At time t=0 the aircraft passes through due north, phi =0. Define the orientation of the body axes relative to F_(H) at this instant as F_(1) The aircraft continues to rotate about an axis pointed toward the ground . Six seconds later the body axes are oriented differently;define this orientation as F_(2)