Skip to main content

Questions tagged [flight-dynamics]

Flight dynamics is the study of the physics driving the performance, stability, and control of aircraft. It is concerned with how forces acting on the aircraft influence its speed, altitude and attitude with respect to time.

5 votes
2 answers
472 views

During flight training rolling on a point aka dutch rolls are an exercise to develop coordination of aileron and rudder to avoid slipping or skidding turns. Why doesn't the heading of the aircraft ...
Chomeh's user avatar
  • 184
0 votes
0 answers
41 views

My question is as the subject conveys, how do I transform between the results? I have tried the obvious way of summing them, but I get a significant discrepancy (~10 %) which I can't overlook without ...
Jan Erik Ludwig Horvath's user avatar
3 votes
3 answers
328 views

I'm trying to create a spreadsheet/calculator that can predict/calculate rate of roll at a range of airspeeds between 0.01 and 0.99 Mach. The goal is to be able to predict an aircraft's roll behavior ...
Ambaryerno's user avatar
2 votes
0 answers
153 views

[This question was inspired by a discussion in chatGPT. ChatGPT is excellent at making cohesive summeries, but from my experience is not so good at explaining/clarifying deep "core issues". ...
user2554's user avatar
  • 169
1 vote
2 answers
271 views

Longer wing allows more efficient planes hence the use of foldable wings. If airport gate dimensions and manufacturing costs were out of the question, what is the most efficient wing length for an ...
Afe's user avatar
  • 1,541
4 votes
2 answers
279 views

The Airbus A220/Bombardier C-series utilizes the C*U fly-by-wire flight control law, which is similar to the ones used in the 777/787. Now, I don't understand much about the C*U flight control laws, ...
A220Lover's user avatar
2 votes
1 answer
217 views

A quick Google search says that the Embraer E2 uses C* for their fly-by-wire control law. Now as far as I understand, C* longitudinal control law commands tracking. So, a neutral stick would command ...
A220Lover's user avatar
8 votes
2 answers
2k views

It's well known that fighter jets can produce vapor condensation when maneuvering aggressively, especially in high-humidity conditions. My question is, can this also happen with smaller aircraft? Is ...
Wyatt's user avatar
  • 4,425
1 vote
0 answers
98 views

My understanding is that lift is approximately proportional to speed, how can planes increase their forward velocity without causing lift?
FourierFlux's user avatar
1 vote
1 answer
340 views

I'm trying to figure out if what I've always thought of as roll from the cockpit is not in fact roll at all. The Tait-Bryan convention defines RPY (roll, pitch, and yaw) as the Euler angles from the ...
Kenn Sebesta's user avatar
  • 6,166
13 votes
1 answer
3k views

I am thinking of a very basic main and tail rotor configuration helicopter, without any aerodynamic surfaces like vertical or horizontal stabilizer, in a steady state horizontal forward flight at ...
Aron's user avatar
  • 131
1 vote
1 answer
216 views

In the PHAK, Chapter 5 Aerodynamics, the following statement is made regarding forces in a climb: The thrust required for a stabilized climb equals drag plus a percentage of weight dependent on the ...
Ryan BW's user avatar
  • 61
1 vote
2 answers
174 views

I'm looking for references for values/formula for lift and drag coenficients. In this paper https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6244461 it is said that $C_L(α)$ and $C_D(α)$ ...
waaat's user avatar
  • 13
6 votes
4 answers
3k views

I've been reading an article on the BBC Website about the 21/May/2024 incident on Singapore Airlines. According to this article: "The rapid changes in G over the 4.6 seconds duration resulted in ...
Stormcloud's user avatar
-4 votes
2 answers
283 views

If two forces are equal and acting in opposite direction should not the object remain stationary. Is there an excess thrust which actually pushes the aircraft forward ?
user75458's user avatar

15 30 50 per page
1
2 3 4 5
18