Relative airflow - Study guides, Class notes & Summaries
Looking for the best study guides, study notes and summaries about Relative airflow? On this page you'll find 573 study documents about Relative airflow.
Page 3 out of 573 results
Sort by
-
ATPL - AGK SET 2 (46/91)verified to pass 2023/2024
- Exam (elaborations) • 11 pages • 2024
- Available in package deal
-
- $17.99
- + learn more
ATPL - AGK SET 2 (46/91)46. Which is a purpose of wing-mounted vortex generators? 
 
A. Reduce the drag caused by supersonic flow over portions of the wing. 
B. Increase the onset of drag divergence and aid in aileron effectiveness at high speed. 
C. Break the airflow over the wing so the stall will progress from the root out to the tip of the wing. - correct answers A. Reduce the drag caused by supersonic flow over portions of the wing. 
 
47. Which is a purpose of wing-mounted vortex generator...
-
ATP CTP Course - Final Test Verified 100% Correct!!
- Exam (elaborations) • 10 pages • 2023
-
- $7.39
- 1x sold
- + learn more
ATP CTP Course - Final Test Questions and Answers 2022. Which of the following statements regarding energy is true? The objective in maneuvering the airplane is to manage energy so that: What is the effect on total drag if airspeed slows below L/D Max? A jet pilot flying at L/D Max will obtain best: When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag predominates? While already at high speed, what happens if Mach is allowed to increase? What is the resu...
-
AFOQT AVIATION EXAM QUESTIONS AND ANSWERS
- Exam (elaborations) • 59 pages • 2023
-
Available in package deal
-
- $13.99
- + learn more
The angle between the chord line of a wing or airfoil and the direction of the relative wind or airflow is called the 
(a) angle of pitch 
(b) degree of roll 
(c) angle of deflection 
(d) angle of attack - Answer- (d) angle of attack 
 
A conventional fixed-wing aircraft is controlled around its longitudinal axis by means of the 
(a) ailerons 
(b) elevators 
(c) rudder 
(d) trim tab - Answer- (a) ailerons 
 
Two statute miles are equal to 
(a) 2.0 nautical miles 
(b) 1.74 nautical miles 
(c)...
-
SCCJA Unit 4 Test with complete solutions| Latest 2024/2025
- Exam (elaborations) • 20 pages • 2024
- Available in package deal
-
- $10.99
- + learn more
SCCJA Unit 4 Test with complete 
solutions. 
Household Members ️ Spouse, former spouse, people with a child in 
common, or a male and female who are/have cohabitating/cohabitated 
Who makes the decision to arrest and prosecute in a DV case? ️ The 
officer 
DV 3rd ️ Causing, or offering/attempting to with the apparent present 
ability to do so, physical harm to a household member 
DV 2nd ️ DV 3rd + special circumstances: Moderate bodily injury (or 
means likely to produce MBI), violation ...
-
ATPL questions and answers 100% Pass
- Exam (elaborations) • 20 pages • 2024
-
- $13.49
- + learn more
ATPL questions and answers 100% Pass 
What are the forces acting on an aircraft in flight? -Answer-Drag. Thrust. Lift and Weight 
What is direct lift control? -Answer-The elevator / stabilizer provide the direct lift control. 
What are high lift devices? -Answer-Trailing edge flaps. Leading edge flaps. Slots 
Define the two major types or Drag. -Answer-Profile and induced drag which equals 
total drag 
What are high drag devices? -Answer-Trailing edge flaps, spoilers, landing gear, revere 
thrus...
Fear of missing out? Then don’t!
-
Gleim Private Pilot FAA Knowledge Test Guide
- Exam (elaborations) • 42 pages • 2023
-
- $17.00
- 1x sold
- + learn more
Gleim Private Pilot FAA Knowledge Test Guide 
 
 
Gleim Private Pilot FAA Knowledge Test Guide 
 
What is one purpose of wing flaps? 
To enable the pilot to make steeper approaches to a landing without increasing the airspeed. 
One of the main functions of flaps during approach and landing is to: 
Increase the angle of descent without increasing the airspeed. 
What is the purpose of the rudder on an airplane? 
To control yaw. 
Which is not a primary flight control surface? 
A. Flaps 
B. Stabilat...
-
NIFE Aerodynamics 2-2-1 Latest Update 100% Pass
- Exam (elaborations) • 5 pages • 2024
- Available in package deal
-
- $9.99
- + learn more
NIFE Aerodynamics 2-2-1 Latest Update 
 
100% Pass 
 
Total drag eqn (Not EO) Dt = Dp + Di 
 
Define Parasite drag and its components Drag that does not aid flight. Has two basic 
elements: form drag and friction drag. Dp = qf 
 
Form drag Results from the disruption of the streamline flow; and the resistance of skin 
friction. Caused by laminar airflow separation from a surface creating a low pressure wake 
behind an object. The pressure differential between the front and rear creates suction t...
-
Mold Test Questions and Answers Already Passed
- Exam (elaborations) • 24 pages • 2024
- Available in package deal
-
- $9.99
- + learn more
Mold Test Questions and Answers 
 
Already Passed 
 
What do the initials RH or RH% stand for? Relative Humidity 
 
What do the initials GPP stand for? Grains per pound/Specific humidity 
 
The initials IICRC stand for what organization? Institute of Inspection , Cleaning Restoration 
Certification 
 
Bound water/moisture is water/moisture that is(circle all that apply): 
a. Water/moisture that can easily be extracted from materials 
b. Water/moisture in structural materials that cannot be remov...
-
SIFT study guide || A Verified A+ Pass.
- Exam (elaborations) • 12 pages • 2024
-
- $11.29
- + learn more
The four forces acting on helicopter in forward flight are...? correct answers Thrust, drag, weight, lift 
 
Bernoulli's Principle or the "venturi effect" correct answers As air flows over upper surface of airfoil, camber (curvature) of airfoil causes increase in speed of airflow which decreased pressure. Pressure is increased on bottom and this gives lift. 
 
Newtons Third Law of Motion and how it applies to helicopters correct answers "for every action there is an equal and opposite reacti...
-
ATPL - AGK SET 2 (46/91)verified to pass 2023/2024
- Exam (elaborations) • 11 pages • 2023
-
Available in package deal
-
- $17.99
- + learn more
ATPL - AGK SET 2 (46/91)46. Which is a purpose of wing-mounted vortex generators? 
 
A. Reduce the drag caused by supersonic flow over portions of the wing. 
B. Increase the onset of drag divergence and aid in aileron effectiveness at high speed. 
C. Break the airflow over the wing so the stall will progress from the root out to the tip of the wing. - correct answers A. Reduce the drag caused by supersonic flow over portions of the wing. 
 
47. Which is a purpose of wing-mounted vortex generator...
Do you wonder why so many students wear nice clothes, have money to spare and enjoy tons of free time? Well, they sell on Stuvia! Imagine your study notes being downloaded a dozen times for $15 each. Every. Single. Day. Discover all about earning on Stuvia