IHS ESDU First approximation to take-off field length of multi-engined transport aeroplanes. 76011

Description
ESDU 76011 gives a method, obtained by correlating flight manual information for 36 aircraft powered by turbo-jet, turbo-fan, turbo-prop or piston engines, for estimating both unfactored all engines operating distance to 35 ft and the balanced field length. The correlation was found to encompass within 8 per cent some 95 per cent of the data. Both distances are correlated using second segment climb gradient as one parameter and a second parameter involving aircraft weight, lift coefficient at take-off safety speed, and thrust. However, for balanced field length a second correlation is given taking into account different levels of deceleration in the stopping phase. A parameter is added to the correlation including the ratio decision speed/take-off safety speed; a correlation for that parameter is also included depending on the average deceleration available during the stopping phase and a table is given of typical values depending on runway condition and braking methods available.
Description
ESDU 76011 gives a method, obtained by correlating flight manual information for 36 aircraft powered by turbo-jet, turbo-fan, turbo-prop or piston engines, for estimating both unfactored all engines operating distance to 35 ft and the balanced field length. The correlation was found to encompass within 8 per cent some 95 per cent of the data. Both distances are correlated using second segment climb gradient as one parameter and a second parameter involving aircraft weight, lift coefficient at take-off safety speed, and thrust. However, for balanced field length a second correlation is given taking into account different levels of deceleration in the stopping phase. A parameter is added to the correlation including the ratio decision speed/take-off safety speed; a correlation for that parameter is also included depending on the average deceleration available during the stopping phase and a table is given of typical values depending on runway condition and braking methods available.

Suppliers

Company
Product
Description
Supplier Links
First approximation to take-off field length of multi-engined transport aeroplanes. - 76011 - IHS ESDU
London, United Kingdom
First approximation to take-off field length of multi-engined transport aeroplanes.
76011
First approximation to take-off field length of multi-engined transport aeroplanes. 76011
ESDU 76011 gives a method, obtained by correlating flight manual information for 36 aircraft powered by turbo-jet, turbo-fan, turbo-prop or piston engines, for estimating both unfactored all engines operating distance to 35 ft and the balanced field length. The correlation was found to encompass within 8 per cent some 95 per cent of the data. Both distances are correlated using second segment climb gradient as one parameter and a second parameter involving aircraft weight, lift coefficient at take-off safety speed, and thrust. However, for balanced field length a second correlation is given taking into account different levels of deceleration in the stopping phase. A parameter is added to the correlation including the ratio decision speed/take-off safety speed; a correlation for that parameter is also included depending on the average deceleration available during the stopping phase and a table is given of typical values depending on runway condition and braking methods available.

ESDU 76011 gives a method, obtained by correlating flight manual information for 36 aircraft powered by turbo-jet, turbo-fan, turbo-prop or piston engines, for estimating both unfactored all engines operating distance to 35 ft and the balanced field length. The correlation was found to encompass within 8 per cent some 95 per cent of the data. Both distances are correlated using second segment climb gradient as one parameter and a second parameter involving aircraft weight, lift coefficient at take-off safety speed, and thrust. However, for balanced field length a second correlation is given taking into account different levels of deceleration in the stopping phase. A parameter is added to the correlation including the ratio decision speed/take-off safety speed; a correlation for that parameter is also included depending on the average deceleration available during the stopping phase and a table is given of typical values depending on runway condition and braking methods available.

Buy Now

Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 76011
Product Name First approximation to take-off field length of multi-engined transport aeroplanes.
Unlock Full Specs
to access all available technical data

Similar Products