Chapter 4, Problem 82P

please find Ix and Iy in mm4, the circles are all hollow and identical

S.4. Yandaki şekilde AB çubuğu pirinç ve CD çubuğu alüminyumdur. Sıcaklık 20°C iken iki çubuk arasında 0,5 mm boşluk bulunmaktadır. a) Sıcaklık 95°C'ye yükseldiğinde çubuklardaki normal gerilmeleri, b) Bu durumda AB ve CD çubuklarındaki deformasyonu bulunuz. AB çubuğu için: E 105 GPa, a = 20x 10 1/°C CD çubuğu için: E-70 GPa, a 23,6x 106 1/°C 0.5 300 250 mm Alüminyum Çap 50 mm Çap 75 mm

Recall the head loss equation developed in class for a sudden expansion (See section 7.7 in your textbook). h₁= (V1-V2)² 2g Show all the steps in going from this equation to equation 3 for the minor loss coefficient, K, above.

Just do Questions 7, 9, 11. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE. (If you have once answered this question don't answer it again I am looking for a difference solution)

This is a tilt and rotation question. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE. I prefer handwritten solutions.

Homework#7

Homework#7

Q3. Consider an inlet flow for an engine with a supersonic inlet Mach number as shown in Figure. below, calculate the total pressure loss between point 1 and 3 if the flow passes first an oblique shock wave and then a reflected shock wave. (30 pts) Моо M∞ = 2.0 && = 30°

Just do Questions 7, 9, 11. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE. (If you have once answered this question don't answer it again)