Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings - Computational and Experimental Investigations
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Bester Preis: Fr. 65.44 ( 66.70)¹ (vom 01.10.2017)
1
9783330652507 - Mujahid Samad Suhaeb: Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings
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Mujahid Samad Suhaeb

Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings

Lieferung erfolgt aus/von: Deutschland DE PB NW

ISBN: 9783330652507 bzw. 3330652500, in Deutsch, Scholar's Press, Taschenbuch, neu.

Fr. 88.20 ( 89.90)¹
versandkostenfrei, unverbindlich
Lieferung aus: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, Agrios-Buch [57449362], Bergisch Gladbach, Germany.
Neuware - When an aircraft is aerodynamically or structurally damaged in battle, it may not able to complete the mission and the damage may cause its loss. The subject of aircraft battle survivability is one of critical concern to many disciplines, whether military or civil. This book considered and focused on Computational Fluid Dynamics predictions and experimental investigations into the effects of simulated battle damage on the low-speed aerodynamics of a finite aspect ratio wing. Results showed that in 2d and 3D CFD simulations, Fluent's® models work reasonably well in predicting jets flow structures, pressure distributions, and pressure-coefficient Cp's contours but not for aerodynamic coefficients. From the experimental results of Finite Wing, the increments for Aspect-ratio, AR6, AR8 and AR10 showed that as damage moves out towards the tip, aerodynamic coefficients increments i.e. lift-loss and drag-rise decreased, and pitching moment-coefficient increment indicated a more positive value at all incidence ranges and at all aspect ratios. Increasing the incidence resulted in greater magnitudes of lift-loss and drag-rise for all damage locations and aspect ratios. 248 pp. Englisch.
2
9783330652507 - Mujahid Samad Suhaeb: Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings
Symbolbild
Mujahid Samad Suhaeb

Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings

Lieferung erfolgt aus/von: Deutschland DE NW

ISBN: 9783330652507 bzw. 3330652500, in Deutsch, neu.

Fr. 65.44 ( 66.70)¹
versandkostenfrei, unverbindlich
Lieferung aus: Deutschland, Lieferzeit: 6 Tage.
When an aircraft is aerodynamically or structurally damaged in battle, it may not able to complete the mission and the damage may cause its loss. The subject of aircraft battle survivability is one of critical concern to many disciplines, whether military or civil. This book considered and focused on Computational Fluid Dynamics predictions and experimental investigations into the effects of simulated battle damage on the low-speed aerodynamics of a finite aspect ratio wing. Results showed that in 2d and 3D CFD simulations, Fluent's® models work reasonably well in predicting jets flow structures, pressure distributions, and pressure-coefficient Cp's contours but not for aerodynamic coefficients. From the experimental results of Finite Wing, the increments for Aspect-ratio, AR6, AR8 and AR10 showed that as damage moves out towards the tip, aerodynamic coefficients increments i.e. lift-loss and drag-rise decreased, and pitching moment-coefficient increment indicated a more positive value at all incidence ranges and at all aspect ratios. Increasing the incidence resulted in greater magnitudes of lift-loss and drag-rise for all damage locations and aspect ratios.
3
9783330652507 - Mujahid Samad Suhaeb: Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings - Computational and Experimental Investigations
Symbolbild
Mujahid Samad Suhaeb

Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings - Computational and Experimental Investigations

Lieferung erfolgt aus/von: Deutschland DE PB NW

ISBN: 9783330652507 bzw. 3330652500, in Deutsch, Scholar's Press, Taschenbuch, neu.

Fr. 79.38 ( 80.91)¹
versandkostenfrei, unverbindlich
Lieferung aus: Deutschland, Versandkostenfrei.
Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings: When an aircraft is aerodynamically or structurally damaged in battle, it may not able to complete the mission and the damage may cause its loss. The subject of aircraft battle survivability is one of critical concern to many disciplines, whether military or civil. This book considered and focused on Computational Fluid Dynamics predictions and experimental investigations into the effects of simulated battle damage on the low-speed aerodynamics of a finite aspect ratio wing. Results showed that in 2d and 3D CFD simulations, Fluent`s® models work reasonably well in predicting jets flow structures, pressure distributions, and pressure-coefficient Cp`s contours but not for aerodynamic coefficients. From the experimental results of Finite Wing, the increments for Aspect-ratio, AR6, AR8 and AR10 showed that as damage moves out towards the tip, aerodynamic coefficients increments i.e. lift-loss and drag-rise decreased, and pitching moment-coefficient increment indicated a more positive value at all incidence ranges and at all aspect ratios. Increasing the incidence resulted in greater magnitudes of lift-loss and drag-rise for all damage locations and aspect ratios. Englisch, Taschenbuch.
4
9783330652507 - Samad Suhaeb, Mujahid: Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings
Symbolbild
Samad Suhaeb, Mujahid

Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings

Lieferung erfolgt aus/von: Deutschland DE PB NW

ISBN: 9783330652507 bzw. 3330652500, in Deutsch, Taschenbuch, neu.

Fr. 87.57 ( 89.26)¹
versandkostenfrei, unverbindlich
Lieferung aus: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, European-Media-Service Mannheim [1048135], Mannheim, Germany.
Publisher/Verlag: Scholar's Press | Computational and Experimental Investigations | When an aircraft is aerodynamically or structurally damaged in battle, it may not able to complete the mission and the damage may cause its loss. The subject of aircraft battle survivability is one of critical concern to many disciplines, whether military or civil. This book considered and focused on Computational Fluid Dynamics predictions and experimental investigations into the effects of simulated battle damage on the low-speed aerodynamics of a finite aspect ratio wing. Results showed that in 2d and 3D CFD simulations, Fluent's® models work reasonably well in predicting jets flow structures, pressure distributions, and pressure-coefficient Cp's contours but not for aerodynamic coefficients. From the experimental results of Finite Wing, the increments for Aspect-ratio, AR6, AR8 and AR10 showed that as damage moves out towards the tip, aerodynamic coefficients increments i.e. lift-loss and drag-rise decreased, and pitching moment-coefficient increment indicated a more positive value at all incidence ranges and at all aspect ratios. Increasing the incidence resulted in greater magnitudes of lift-loss and drag-rise for all damage locations and aspect ratios. | Format: Paperback | Language/Sprache: english | 248 pp.
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9783330652507 - Mujahid Samad Suhaeb: Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings: Computational and Experimental Investigations
Mujahid Samad Suhaeb

Aerodynamics of Battle-Damaged Finite Aspect Ratio Wings: Computational and Experimental Investigations (2017)

Lieferung erfolgt aus/von: Deutschland EN PB NW

ISBN: 9783330652507 bzw. 3330652500, in Englisch, 248 Seiten, Scholars' Press, Taschenbuch, neu.

Fr. 76.86 ( 78.34)¹
versandkostenfrei, unverbindlich
Lieferung aus: Deutschland, Versandfertig in 1 - 2 Werktagen, Versandkostenfrei.
Von Händler/Antiquariat, dodax-shop-eu.
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