ATP CTP Course REAL EXAM 2023/2024 QUESTIONS AND EXPERT VERIFIED ANSWERS ALREADY GRADED A GUARANTEED PASS ASSURED
8 mal angesehen 1 mal verkauft
Kurs
ATP CTP Course
Hochschule
ATP CTP Course
ATP CTP Course REAL EXAM 2023/2024
QUESTIONS AND EXPERT VERIFIED ANSWERS
ALREADY GRADED A GUARANTEED PASS
ASSURED
Which of the following statements regarding energy is true?
A. Kinetic energy decreases with increasing airspeed
B. Potential energy is approximately proportional to airspeed
C. ...
which of the following statements regarding energy
Schule, Studium & Fach
ATP CTP Course
ATP CTP Course
Verkäufer
Folgen
Onlystudents
Deine Reviews
Inhaltsvorschau
onlystudents
ATP CTP Course REAL EXAM 2023/2024
QUESTIONS AND EXPERT VERIFIED ANSWERS
ALREADY GRADED A GUARANTEED PASS
ASSURED
Which of the following statements regarding energy is true?
A. Kinetic energy decreases with increasing airspeed
B. Potential energy is approximately proportional to airspeed
C. Chemical Energy remains constant throughout flight
D. Kinetic energy can be traded for potential energy and potential energy can be traded for
kinetic energy
D. Kinetic energy can be traded for potential energy and potential energy can be traded for
kinetic energy
The objective in maneuvering the airplane is to manage the energy so that:
A. Kinetic energy stays between limits (stall and placards)
B. Potential energy stays between limits (terrain and buffet altitude)
C. Chemical energy stays above certain thresholds (not running out of fuel)
D. All of the above
D. All of the above
What is the effect on total drag if airspeed slows below L/DMax?
A. Drag increases because of increased parasite drag.
B. Drag decreases because of lower induced drag.
C. Drag increases because of increased induced drag.
C. Drag increases because of increased induced drag
A jet pilot flying at L/DMax will obtain best:
A. Range
B. Endurance
C. Ride Quality
,onlystudents
B. Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag
predominates?
a. Parasite
b. Induced
c. Each type of drag contributes equally
a. Parasite
While already at high speed, what happens if Mach is allowed to increase?
a. Airflow over parts of the airplane begin to exceed the speed of sound
b. Shock waves can cause local airflow separation
c. Characteristics such as pitch-up, pitch-down, or buffeting may occur.
d. All of the above
d. All of the above
What is the result of a shock-induced separation of airflow occurring symmetrically near the
wing root of a swept wing aircraft?
a. A high-speed stall and sudden pitch-up
b. Severe porpoising.
c. A severe moment or "Mach Tuck".
c. A severe moment or "Mach Tuck".
The speed of sound generally decreases with increasing altitude. This occurs because:
a. The air temperature decreases.
b. The air pressure decreases.
c. The composition of the air changes.
a. The air temperature decreases.
Critical Mach number can be defined as:
a. The speed at which the aircraft is traveling faster than sound.
b. The maximum Mach number at which an aircraft may be safely operated.
c. the speed of an aircraft in which airflow over any part of the aircraft or structure first reaches,
but doesn't exceed, Mach 1.0
, onlystudents
c. the speed of an aircraft in which airflow over any part of the aircraft or structure first reaches,
but doesn't exceed, Mach 1.0
Stability in the vertical axis tends to drive the sideslip angle toward zero. The most dynamic
stability about the vertical axis on modern jet transports is from:
a. The vertical fin
b. The rudder
c. An active stability augmentation system/yaw damper
d. Pilot roll input
c. An active stability augmentation system/yaw damper
Swept wings cause a significant:
a. increase in effectiveness of flaps.
b. Reduction in effectiveness of flaps
c. flap actuation reliability issue
b. Reduction in effectiveness of flaps
Why is convergence of Stall AOA and MMO hazardous?
a. Any decrease in airspeed will cause the aircraft to buffet and potentially stall
b. Any increase in airspeed will cause the aircraft to buffet and potentially cause Mach Tuck
c. Airspeed changes may occur due to environmental factors, without pilot input.
d. All of the above
d. All of the above
To maintain altitude in a banked turn, the lift produced by an airplane must be:
a. Greater than the airplane weight, and the amount is a function of bank angle
b. Greater than the airplane weight, and the amount is a function of altitude
c. Equal to the weight of the airplane
a. Greater than the airplane weight, and the amount is a function of bank angle
Alle Vorteile der Zusammenfassungen von Stuvia auf einen Blick:
Garantiert gute Qualität durch Reviews
Stuvia Verkäufer haben mehr als 700.000 Zusammenfassungen beurteilt. Deshalb weißt du dass du das beste Dokument kaufst.
Schnell und einfach kaufen
Man bezahlt schnell und einfach mit iDeal, Kreditkarte oder Stuvia-Kredit für die Zusammenfassungen. Man braucht keine Mitgliedschaft.
Konzentration auf den Kern der Sache
Deine Mitstudenten schreiben die Zusammenfassungen. Deshalb enthalten die Zusammenfassungen immer aktuelle, zuverlässige und up-to-date Informationen. Damit kommst du schnell zum Kern der Sache.
Häufig gestellte Fragen
Was bekomme ich, wenn ich dieses Dokument kaufe?
Du erhältst eine PDF-Datei, die sofort nach dem Kauf verfügbar ist. Das gekaufte Dokument ist jederzeit, überall und unbegrenzt über dein Profil zugänglich.
Zufriedenheitsgarantie: Wie funktioniert das?
Unsere Zufriedenheitsgarantie sorgt dafür, dass du immer eine Lernunterlage findest, die zu dir passt. Du füllst ein Formular aus und unser Kundendienstteam kümmert sich um den Rest.
Wem kaufe ich diese Zusammenfassung ab?
Stuvia ist ein Marktplatz, du kaufst dieses Dokument also nicht von uns, sondern vom Verkäufer Onlystudents. Stuvia erleichtert die Zahlung an den Verkäufer.
Werde ich an ein Abonnement gebunden sein?
Nein, du kaufst diese Zusammenfassung nur für 17,70 €. Du bist nach deinem Kauf an nichts gebunden.
