AVIA 305 Quiz Airspeed Airfoils
AVIA 305 Quiz: Airspeed, Airfoils, Lift, and Drag Results for Joshua Hahn A 22,492 lb. aircraft has a (L/D)max value of 9.5; find its minimum drag. An aircraft is traveling…
AVIA 305 Quiz Maneuvering Performance
AVIA 305 Quiz: Maneuvering Performance Covers the Learn material from Module 5: Week 5 — Module 6: Week 6. Dynamic hydroplaning Directional control during a crosswind takeoff in a C172…
AVIA 305 Quiz Aircraft Performance
AVIA 305 Quiz Aircraft Performance Covers the Learn material from Module 3: Week 3 — Module 4: Week 4. As altitude increases, power available from a turboprop engine: (Reference Figure…
AVIA 305 Test 4
AVIA 305 Test 4 Liberty University In Subsonic flight the air is considered to be A Normal shock wave will have what effect on velocity and Mach number? Aircraft speeds…
AVIA 305 Test 3
AVIA 305 Test 3 Liberty University Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift – Angle of Attack (AOA)…
AVIA 305 Test 2
AVIA 305 Test 2 Liberty University The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is If the weight of a jet…
AVIA 305 Test 1
AVIA 305 Test 1 Liberty University 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…
AVIA 305 Research Paper
AVIA 305 Research Paper Liberty University The student will submit a 4–6-page research paper on the unique aerodynamic characteristics of his/her favorite aircraft. The paper must adhere to current APA…