Avia 305 test - Study guides, Class notes & Summaries

AVIA 305 Test Prep UPDATED Exam Questions and CORRECT Answers An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940. - CORRECT ANSWER- Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension

An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940. correct answers Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension D = 0.940 X 300lbs D = 282lbs Lift: Sin 20° = L/T (Rearrange) Lift = Sin 20° X Tension Lift = 0.342 X 300 lbs Lift...

AVIA 305 Test 3 Prep Study Guide Exam. CHAPTER 12 - CORRECT ANSWER Slow‐Speed Flight The main difference between the Cl - a curves for straight‐wing aircraft is that - CORRECT ANSWER the swept‐wing aircraft has a lower value of CL(max). the straight‐wing aircraft does not fly at as high an AOA for CL(max) the swept‐wing aircraft does not have an abrupt loss of lift at CL(max) Low‐speed stall will start at the wing's trailing edge - CORRECT ANSWER Where C1/CL is a ma...

LU AVIA 305 Test 3 • Question 1 2.5 out of 2.5 points Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. For a safe takeoff, the Critical Field Length must be no greater than the runway available An increase in density altitude has what effect on takeoff performance

AVIA 305 TEST 1 2021/2022 Correct answers are hidden. Score for this quiz: 65 out of 75 Submitted Jan 21 at 7:33pm This attempt took 53 minutes. IncorrectQuestion 1 0 / 2.5 pts A slotted flap is an example of a(n) (Ref Figure 1) Camber changer Energy adder Area changer A & B Question 2 2.5 / 2.5 pts

AVIA 305 Test 3 • Question 1 Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. • Question 2 For a safe takeoff, the Critical Field Length must be no greater than the runway available • Question 3 An...

AVIA 305 Review Test Submission: Test 1 Attempt Score 57.5 out of 75 points • • Question 1 An airplane is operating from an airfield that has a barometric pressure of 28.86 in. Hg and a runway temperature of 20C. Calculate (or find in Table 2.1) the Temperature Ratio: • Question 2 The corrections that must be made to indicated airspeed (IAS) to obtain calibrated airspeed (CAS) are: • Question 3 A large Reynolds number (greater than 10 million) indicates • Question 4 An airplane is oper...

AVIA 305 TEST 2 2021/2022 AVIA 305 Test 2 User Course LUO Test Test 2 Status Completed Attempt Score 67.5 out of 75 points • Question 1 2.5 out of 2.5 points The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is Selected Answer: Less • Question 2 If the weight of a jet airplane is increased then 2.5 out of 2.5 points Selected Answer: Induced drag increases more than parasite drag • Question 3 An example of a power-producing airc...