Why Does Low Level, High Speed Flight Decrease Aircraft Efficiency?

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Discussion Overview

The discussion centers on the reasons behind the decrease in aircraft efficiency, specifically the aerodynamic and engine efficiency, during low-level, high-speed flight. It explores concepts related to drag, altitude, and speed in the context of aircraft design and performance.

Discussion Character

  • Exploratory, Technical explanation, Conceptual clarification

Main Points Raised

  • One participant references a statement from a book regarding the reduction of aerodynamic efficiency at low-level, high-speed flight.
  • Another participant suggests looking into why airliners operate at high altitudes, mentioning factors like 'wave drag' and 'critical mach number' as relevant to speed.
  • A later reply provides an explanation that drag increases with the square of airspeed and also with increasing air density, noting that low altitudes have higher air density, which contributes to increased drag during level flight.

Areas of Agreement / Disagreement

Participants present various explanations and factors affecting aircraft efficiency, but there is no consensus on a singular reason or model. Multiple perspectives on the relationship between altitude, speed, and drag remain in discussion.

Contextual Notes

The discussion does not resolve the complexities of the interactions between drag, altitude, and speed, nor does it clarify the definitions of terms like 'wave drag' or 'critical mach number'.

kevjcarvalho
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hey,
I was reading Aircraft Design: A Conceptual Approach by Raymer and i came across the following line.
' The aerodynamic efficiency of an aircraft, expressed as the lift to drag ratio is greatly reduced during low level, high speed flight as well is its engine efficiency. '
Can someone tell me why. Thanks.
 
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Search for the reason Airliners fly at 30,000ft during cruise.
and, as far as speed is related, you must be aware of the 'wave drag' and 'critical mach number'.
 
Thanks.
 
Here's a bit more explanation: 1) drag increases with the square of airspeed 2) drag also increases with increasing air density. Air density is the highest near sea level and then decreases the higher you go. So at low altitudes and high speeds, that's the worst possible combination from a drag perspective because it maximizes drag in level flight. We could further expound on all this but that's a basic explanation to Raymer's statement.
 

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