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Questions tagged [performance-calculation]

Questions about calculating the various measures of performance of an aircraft.

1 vote
1 answer
89 views

I'm trying to find a reason for a 1.15 defactoring when it appears that the 1.3 factor on ASDA must always be more limiting. Referencing this: CAT.POL.A.305 Take-off ... (b) The unfactored take-off ...
ExternalUse's user avatar
2 votes
5 answers
788 views

Is there a name for the airspeed at which the wings(at a 0 degree AOA) of an airplane start to generate enough lift to lift the aircraft up to its own weight(balanced)?
gbe's user avatar
  • 8,485
2 votes
4 answers
396 views

If I have a jet engine producing say 650N of thrust, could that engine in the right airframe fly at Mach 2 or Mach 1? What, apart from the airframe limitations, determines the maximum speed it will ...
user116241's user avatar
0 votes
1 answer
126 views

I am a Military Helicopter pilot. I’ve been inputting MSL instead of Pressure altitudes of LZs into my performance charts for Power available calculations. The Pressure altitude is not always ...
Tyler Hoogervorst's user avatar
6 votes
2 answers
293 views

Hello Aviation community! I am currently in the (lift-dependent) induced drag calculation of my aircraft design lecture where I came upon this slide: As the title suggests, I am not sure exactly ...
CheesyBeqa's user avatar
2 votes
3 answers
303 views

[1966 Cessna 172G Cruise chart] In the shown Cruise performance chart it states that it is standard conditions. If a normal lapse rate at 7,500 ft is 0 celsius how would I see accurate values if my ...
Wes's user avatar
  • 641
6 votes
1 answer
268 views

I know that I have asked similar question recently, but I still don't have a good answer. I noticed that (on a 737 NG/MAX) when we switch on PACKs during Before Taxi Procedure or for the APU, the take-...
Konrad's user avatar
  • 2,227
4 votes
1 answer
562 views

Could somebody explain impact of bleed air extract from engines on take-off N1 and EGT? As far as I know (considering 737NG) using engine bleed air decreases calculated N1 for take-off by the FMC, ...
Konrad's user avatar
  • 2,227
3 votes
1 answer
650 views

Assuming everything in the aircraft is a non consumable and does not move during the flight, is the cg shape dependent on the fuel storage? I understand the cg has limits, but what determines the ...
Wes's user avatar
  • 641
3 votes
1 answer
149 views

When calculating the landing distance the QRH says the approach is flown at VREF30 + 20. As well as the landing must be conducted with Flaps 20. The performance tables say to add 200 ft per 5 kts ...
user102948's user avatar
0 votes
1 answer
198 views

TALPA - Takeoff and Landing Performance Assessment has been introduced. What is it exactly and why is it not used for take-off, when it is stated in the name TALPA?
Ted Staggs's user avatar
2 votes
1 answer
145 views

I have designed an aircraft and wanted to determine its performance charachteristics. the following parameters have been utilised: aircraft specifications: Mtow = 1.7kg wing_area = 0.411 m^2 Cl_max = ...
Curiousraptor's user avatar
1 vote
1 answer
662 views

If you are flying to the most remote airport(according to simple flying most remote airport is Mataveri International Airport), while flying on a typical airliner with normal weather, in the event of ...
gbe's user avatar
  • 8,485
1 vote
1 answer
341 views

I would like to determine the amount of fuel required for a flight at a given range/payload combination - ideally from the payload/range-diagram [1] of the corresponding aircraft alone. I know that ...
Wasserwaage's user avatar
  • 1,976
0 votes
2 answers
903 views

I am using a takeoff performance application that seems to prioritize a higher V1 speed whenever there is extra runway available. It does this as long as the Acceleration-Stop Distance (ASD) remains ...
alQ's user avatar
  • 75

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