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Modification of Delta Wing Leading Edge with Rectangular Slots: A Key to Improved Delta Wing Efficiency - Softcover
Synopsis
Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification.
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Modification of Delta Wing Leading Edge with Rectangular Slots: A Key to Improved Delta Wing Efficiency
Published by
LAP LAMBERT Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Softcover
Seller: Ria Christie Collections, Uxbridge, United Kingdom
Seller rating 5 out of 5 stars
Condition: New. In. Seller Inventory # ria9786208419547_new
Quantity: Over 20 available
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Modification of Delta Wing Leading Edge with Rectangular Slots (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Paperback
Seller: CitiRetail, Stevenage, United Kingdom
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Seller Inventory # 9786208419547
Quantity: 1 available
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Modification of Delta Wing Leading Edge with Rectangular Slots: A Key to Improved Delta Wing Efficiency
Published by
LAP LAMBERT Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Softcover
Seller: California Books, Miami, FL, U.S.A.
Seller rating 5 out of 5 stars
Condition: New. Seller Inventory # I-9786208419547
Quantity: Over 20 available
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Modification of Delta Wing Leading Edge with Rectangular Slots
Published by
LAP LAMBERT Academic Publishing Jan 2025, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Taschenbuch
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 60 pp. Englisch. Seller Inventory # 9786208419547
Quantity: 2 available
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Modification of Delta Wing Leading Edge with Rectangular Slots : A Key to Improved Delta Wing Efficiency
Published by
LAP LAMBERT Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Taschenbuch
Seller: AHA-BUCH GmbH, Einbeck, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification. Seller Inventory # 9786208419547
Quantity: 1 available
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Modification of Delta Wing Leading Edge with Rectangular Slots (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Paperback
Seller: AussieBookSeller, Truganina, VIC, Australia
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability. Seller Inventory # 9786208419547
Quantity: 1 available
Seller Image
Modification of Delta Wing Leading Edge with Rectangular Slots
Published by
LAP LAMBERT Academic Publishing Jan 2025, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Taschenbuch
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification.Books on Demand GmbH, Überseering 33, 22297 Hamburg 60 pp. Englisch. Seller Inventory # 9786208419547
Quantity: 1 available
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Modification of Delta Wing Leading Edge with Rectangular Slots (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6208419549
ISBN 13: 9786208419547
New
Paperback
Seller: Grand Eagle Retail, Mason, OH, U.S.A.
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. Delta wing is proved to be suitable for high speed subsonic and supersonic flights. At the other end it gives unique structural advantages and aerodynamic characteristics. Many design variation has been evolved over the years within and without additional stabilizing surfaces. The main aim of the Project is to find how much energy is utilized in this flow with respect to the lift coefficient and other factors. Not only finding the experimental values along with those CFD simulations with CATIA and ANSYS are to be recorded. Here we have two modification. The first modification are with 6 slots and the other with 8 slots. Each slots are measured to be in 6x2mm. So based on the performance of the fighters these shapes are incremented with reference to all the summaries. By comparing all these results and it is to be concluded whether if it is efficient and real life design can be evolved with these leading edge modification. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Seller Inventory # 9786208419547
Quantity: 1 available