Questions tagged [airspeed]

The speed of an aircraft relative to the air. Among the common conventions for qualifying airspeed are: indicated airspeed ("IAS"), calibrated airspeed ("CAS"), true airspeed ("TAS"), equivalent airspeed ("EAS") and density airspeed.

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Why the ADS-B out doesn't broadcast the True air speed in its ES message?

The ASTERIX (version 2.1) items of ADS-B GS cat 21 contain True air speed but when we check the Asterix data that we recieved by GS we did not find the True air speed value, why ?
Uniform's user avatar
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Is it possible to calculate Calibrated Airspeed from True Airspeed, Temp, and Pressure Altitude? [duplicate]

Looking at a digital E6B, there is a function for calculating CAS that I am trying to recreate and program myself. Inputs: Pressure Altitude Temp in Celcius True Airspeed Outputs: CAS Mach # ...
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How to Calculate Required True Airspeed to maintain desired ground speed?

Working on programming my own E6B and am stuck trying to calculate the following problem from Sporty's E6B: Given wind info and desired speed/course, what airspeed/heading should I have in order to ...
Bellarose143's user avatar
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Why do all trend vectors in the G1000 on airplanes indicate the status 6 seconds later? Why 6? Why not 5 or 10?

Why do all trend vectors in the G1000 on airplanes indicate the status 6 seconds later? Why 6? Why not 5 or 10? The fact that the trend vector shows after 6 seconds allows us to turn 3 degrees per ...
pilot162's user avatar
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How can TAS be calculated from indicated temperature and Mach number? [duplicate]

Situation I am working on programming my own E6B while I learn more about aviation, but I have run into some confusion. Two pairs of the equations are very similar except for using true or indicated ...
Bellarose143's user avatar
4 votes
4 answers
375 views

Why does an aircraft require less power when it is flying slower than the most efficient speed?

While I understand the derivation of Power required, I fail to understand why minimum power required corresponds to a velocity that is lower than velocity corresponding to minimum thrust required. My ...
Akshay Kashyap Panda's user avatar
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Why isnt the structure of the aircraft affected by high true air speeds or high ground speeds?

Let's suppose that in Cruise flight I exceed the VNE in TAS or in ground speed, why isn't the structure of the aircraft affected by the high speeds? I am sorry for my english, I am not a native ...
Andres's user avatar
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Why does elevator trim hold a given airspeed? [duplicate]

I'm trying to understand a principle described in the book Stick and Rudder by Wolfgang Langewiesche between angle of attack and airspeed in relation to the elevator trim. He states that as angle of ...
RattMuscle's user avatar
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how to calculate wind speed and direction using flight data, at some latitude and longitude? [duplicate]

I have a data file which has the aircraft state details with latitude and longitude recorded for certain radius. Now, I'm trying to calculate wind direction and wind speed. Example: At lat=41 and long ...
Siva's user avatar
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Mathematically calculate Mach number using CAS and PA WITHOUT flight computer

I am just wondering how to calculate the Mach number from CAS and Pressure Altitude WITHOUT the use of a flight calculator. E.g Given FL300 (30000ft) and 325kt CAS find and Mach number. I have always ...
Steven Shen's user avatar
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Why use indicated airspeed instead of dynamic pressure [closed]

It uses the difference between total pressure and static pressure, provided by the system, to either mechanically or electronically measure dynamic pressure. The dynamic pressure includes terms for ...
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Is my airspeed calculation code correct?

Not sure if I should ask here, on Drones SE, or on Code Review SE. Is my Python code for calculating airspeed given ground speed, ground direction, wind speed, and direction from which the wind is ...
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Speed change in IFR flight in class C or D airspace

Can I change speed while flying IFR in class C or D airspace without having a clearance from ATC? I tried to find it in some documents on EASA website but I did not find anything.
Filip Adam's user avatar
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Should the approach speed and wind be changed below 700ft on an A320?

The FCOM says: When managed, the speed target is computed by the FMGS and may be modified by the flight crew through the MCDU. At 700 ft RA, the current speed target value is memorized by the ...
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Does the reduced aerodynamic damping at higher altitudes affect the Vno (maneuvering speed) of an airplane?

Since reduced aerodynamic damping at higher altitudes reduces the needed control input for maneuvers, is this just about the required force to move the controls or also about the speed of the ...
Erik Stens's user avatar
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1 answer
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Why does true airspeed decrease with altitude?

I was having a discussion with a friend who's going for a record speed over distance attempt. We were discussing which altitude will have the fastest TAS, and I suggested it would be the highest ...
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Air density factor when calculating Airspeed

I am making my own attitude indicator / AHRS, like a Garmin G5. I am using two pressure sensors to measure altitude & airspeed via static /pitot lines. Now I know the formula for calculating ...
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Does optimum IAS for climb vary with altitude?

I was in an argument about aerodynamics and we eventually derived an equation as follows. So I'm going by this equation: $$RoC = \frac{\eta_p P-VD}{W}$$ Where $\eta$ represents propeller efficiency. ...
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2 answers
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How to determine the maximum forward airspeed of a plane in an unaccelerated flight?

What is the equation needed to determine the maximum forward airspeed of a propeller driven plane in an unaccelerated level flight? I need an example with units of measurements. The engine is rated at ...
Justintimeforfun's user avatar
3 votes
3 answers
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Changing the missile's flight speed

I am interested in the range of velocity changes of missiles. Planes have a minimum speed set equal to the landing speed, helicopters also have a set speed - this is zero, but what about missiles? ...
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What is the speed of anti-ice bleed airflow in helicopter turboshaft engines?

If we consider the most modern turboshaft engines, what will the approximate speed for the bleed airflow when it's routed from the latter stages of the engine and supplied to the areas that require ...
Arthur C's user avatar
-8 votes
2 answers
164 views

What about measuring airspeed from control surface forces on the framework?

I watch a lot of these videos that people make about air disasters. One factor that seems (or hopefully seemed) to crop up is where pilots get hopelessly confused about airspeed, particularly (it ...
mike rodent's user avatar
3 votes
1 answer
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Significance of $\frac{C_L^{3/2}}{C_D}$

I am aware that this value of lift coeff. over drag coeff. occurs when the zero lift drag is 3X the drag due to lift, and that this will correspond to a specific airspeed. What is the significance of ...
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Confused about best range speed and Carson speed

I have read that best lift /drag ratio gives maximum range which makes perfect sense to me. I have also read Carson speed gives the best fuel consumption. which doesn’t make sense because this would ...
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Does Indicated Stall speed increase with altitude (Coffin Corner)?

It is my understanding that Indicated Stall speed is mostly constant with altitude, the one that increases is True Stall Speed. Given that PFD show speed as IAS, how come the yellow speed range ...
Max the head's user avatar
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3 answers
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What is the general mathematical relationship between increasing an airplane's weight and the needed thrust to fly?

I understand that increasing an aircraft's weight without changing any other properties means that its takeoff, stall and cruising speeds all increase since you need to generate additional lift. So ...
J-bob's user avatar
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2 answers
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How is a "turning polar" constructed?

To start with something familiar: here's a flight polar. As we learned, the best glide speed is found by starting at the 0,0 point, and drawing a line tangent to the sink rate line. The intersection ...
Xpector's user avatar
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How is CAS ans GS affected by instant wind changes at different altitudes

Okay, a theoretical example here which I hope will help me understand the physics better. Conditions: Altitude: 50 ft (over sea) GS: 300 knts CAS: 300 ktns Wind: 0 If I now get a 10 knts head wind (...
Jesper.Lindberg's user avatar
2 votes
1 answer
393 views

How to compute the airspeed change based on the Altitude change

The plot shows that: when I fly with fixed MACH, the true air speed decreases when the altitude increase; when I fly with fixed CAS, the true airspeed increases when altitude increase. So how could I ...
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Airspeed change in wind shear

The instrument questions I’m studying say that a decreasing tailwind will increase airspeed. I can’t wrap my head around why this would be the case.
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TAS from POH or e6b

I always calculated my TAS at any cruise altitude by Using my planned cruise (pressure) altitude, temperature Plug desired CAS, PA, temperature into e6b and get TAS But I've also seen people get TAS ...
Jonathan's user avatar
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Please describe ram pressure in simple terms [duplicate]

Please someone describe the following sentence in simple words: The Airspeed Indicator is calibrated for 'standard' sea level density, so it will only read TAS if the density of the air through which ...
Kqt's user avatar
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2 answers
343 views

Modern method to verify speed of a homebuilt aircraft

Summary: In 2001, airspeed of homebuilt aircraft was calculated by flying in a ⊔-shape and using trigonometry to subtract wind effects. Now that we have portable computers, is there a more modern ...
Zaz's user avatar
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What is the green arrow on the 777's airspeed tape? Does it exist on other types as well?

Image source: fsnews.eu I found this green arrow on the primary flight display (PFD) of a 777. What does it show? I'm assuming it's for showing acceleration and deceleration but I am not too sure. Is ...
Aviation Enthusiast's user avatar
4 votes
1 answer
306 views

Calculating airspeed by flying in a U shape: Horseshoe Heading Technique

I saw some equation in a log recently and I believe it went something as follows: $v_1$ : flying North, $\ \ v_2$ : flying West, $\ \ v_3$ : flying South. $$ \text{TAS} = \frac 1 2 \sqrt{v_1^2+v_2^2+...
Zaz's user avatar
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9 votes
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Strange airspeed indicator in the Douglas X-3 Stiletto

The cockpit of the Douglas X-3 Stiletto has a rather weird looking airspeed indicator. (The leftmost instrument in the top row.) Two concentric circular scales, the outer one goes from 0 to 20, the ...
tml's user avatar
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-1 votes
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Why airflow travels faster on upper wings?

I have been looking for solutions and come up with two popular explanations: Conservation of mass / Continuity For a positive-cambered wing, the streamlines would be compressed/converged at the ...
Raymond Anderson's user avatar
3 votes
3 answers
3k views

Power calculation of propeller

This is probably a very simple question, but I have been really struggling and need your help. I have simulated a propeller with these parameters on Ansys: Thrust: 2000 N Angular Velocity: 314 rad/s ...
P Ek's user avatar
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6 votes
3 answers
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Do pitot tubes account for reduced pressure at altitude?

Do pitot tubes account for reduced pressure at altitude? Does indicated airspeed reduce with altitude? If so, how much? Is it different for small planes vs big commercial airliners?
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0 answers
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How are IAS/CAS and TAS used in flight?

Could you please explain to me one moment in relation to IAS and TAS. In all books I read I see that the IAS is highlighted as a reference for stall, take-off, landing and other performance items. So, ...
Sergey's user avatar
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3 votes
2 answers
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How can an ultralight be slowed down for landing in a tailwind?

When flying an ultra light and I have a tail wind, and, with the engine at idle how do I slow down to land ?
Redderk's user avatar
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7 votes
1 answer
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What is the difference between Vs and Vs1g?

As the name suggests, what is the difference between Vs1g and Vs? If both of them are referring to the stall condition, why they aren't the same? Which one is usually greater and why? Why do we need a ...
Darjan's user avatar
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What's the penalty for exceeding 250 kts below 10,000 ft MSL without authorization?

What if any enforcement actions by the FAA are likely for exceeding the 250 KIAS limitation below 10,000 ft MSL?
vector's user avatar
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4 votes
2 answers
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Ground Speed vs True Airspeed from Departure Point to Destination - time interval

Looking at navigation theory right now and I'm stuck in the understanding of TAS and GS. How does GS determine the time interval it takes for an aircraft to fly from the DP to the DEST, if TAS ...
JandyPilot's user avatar
2 votes
1 answer
322 views

How can I calculate 'Max aircraft Load Factor' and 'Max aircraft Speed' when flaps are fully extended on a civil aircraft? [closed]

I am trying to calculate the critical loading conditions for Flaps (in order use them inside my Finite Element Analysis to, determine if the Flaps will be able to bear these critical loads) during the ...
Rameez Ul Haq's user avatar
2 votes
1 answer
184 views

How can PreciseFlight speedbrakes double the drag while being so small?

Look at this photo of some PreciseFlight© speed brakes: On the website it is claimed that these little red plates can double drag and descent rates. I cannot believe that. Can this be true, and if ...
TheEagle's user avatar
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-3 votes
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If the altitude of the aircraft is given by the pitot tube, in icing condition with heat on, how is real altitude /speed interpretation done? [duplicate]

If the altitude of the aircraft is given by the pitot tube, in icing condition with pitot heat on how is real altitude /speed interpretation done? Because the air density and temperature is not ...
George Geo's user avatar
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What is propeller pitch speed?

I was using Ecalc to calculate some flight parameters and then I came across this term called "propeller pitch speed". Can anyone explain me what this means?
Deepu Johnson's user avatar
1 vote
2 answers
226 views

What are the relations between Angle of attack and Calibrated Airspeed?

I would like to estimate Angle of Attack using trigonometric relations i.e AoA = arctan (w/u) airspeed components (i.e u, v, w). When I am considering body 'x' velocity ('u' component), is it ...
S.Prabhu's user avatar
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Do aircraft travel faster at higher altitudes?

I'm aware of the difference between TAS and IAS, and how IAS gets lower in reference to TAS as you climb and the air gets thinner. What I'm trying to figure out is whether or not an aircraft's IAS ...
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