Links So first, I really liked this website, until I figured out that there were bots that steals the points from you, and were never moderated. I strongly believe that the moderators of should ban the use of any domains (if that’s what you call it). For example, things that ends with “.com” shouldn’t be allowed. I’ve heard that by clicking into one of those Bitly links, you might risk getting a virus, which Bucks bad for the people who are new to this website. I believe that this website is great, but virus bots are ruining it. I might even have to quit because of them ):

***To make this educational, what is 0.5(28)?***

Thank you for reading my rant. Sorry to any moderators who find this uneducational... I just found the bots really disturbing, and it would be really nice of you guys if you can help us with this

Thank you~

Write an equation in point-slope form for the line through the given point that has the given slope (-2,-7); m=-3/2

Airplane speeds are measured in three different ways: (1) indicated speed, (2) true speed, and (3) ground speed. the indicated airspeed is the airspeed given by an instrument called an airspeed indicator. a plane’s indicated airspeed is different from its true airspeed because the indicator is affected by temperature changes and different altitudes of air pressure. the true airspeed is the speed of the airplane relative to the wind. ground speed is the speed of the airplane relative to the ground. for example, a plane flying at a true airspeed of 150 knots into a headwind of 25 knots will have a ground speed of 125 knots. the problems below refer to static and dynamic pressure. static pressure is used when a body is in motion or at rest at a constant speed and direction. dynamic pressure is used when a body in motion changes speed or direction or both. a gauge compares these pressures, giving pilots an indicated airspeed. in problem #s 1 and 2, use the following information. the indicated airspeed s (in knots) of an airplane is given by an airspeed indicator that measures the difference p (in inches of mercury) between the static and dynamic pressures. the relationship between s and p can be modeled by s=136.4p√+4.5. 1. find the differential pressure when the indicated airspeed is 157 knots. 2. find the change in the differential pressure of an airplane that was traveling at 218 knots and slowed down to195 knots. in problem #s 3 and 4, use the following information. the true airspeed t (in knots) of an airplane can be modeled by t=(1+a50,000) ⋅ s, where a is the altitude (in feet) and s is the indicated airspeed (in knots). 3. write the equation for true airspeed t in terms of altitude and differential pressure p. 4. a plane is flying with a true airspeed of 280 knots at an altitude of 20,000 feet. estimate the differential pressure. explain why you think your estimate is correct.

You have 138.72 in your saving account u take out 45.23 and 18.00 you deposit 75.85 into your account