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.
"Sinopsis" puede pertenecer a otra edición de este libro.
EUR 7,65 gastos de envío en Estados Unidos de America
Destinos, gastos y plazos de envíoLibrería: Best Price, Torrance, CA, Estados Unidos de America
Condición: New. SUPER FAST SHIPPING. Nº de ref. del artículo: 9786208419547
Cantidad disponible: 2 disponibles
Librería: Grand Eagle Retail, Mason, OH, Estados Unidos de America
Paperback. Condición: 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. Nº de ref. del artículo: 9786208419547
Cantidad disponible: 1 disponibles
Librería: California Books, Miami, FL, Estados Unidos de America
Condición: New. Nº de ref. del artículo: I-9786208419547
Cantidad disponible: Más de 20 disponibles
Librería: Ria Christie Collections, Uxbridge, Reino Unido
Condición: New. In. Nº de ref. del artículo: ria9786208419547_new
Cantidad disponible: Más de 20 disponibles
Librería: Books Puddle, New York, NY, Estados Unidos de America
Condición: New. Nº de ref. del artículo: 26404612031
Cantidad disponible: 4 disponibles
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 60 pp. Englisch. Nº de ref. del artículo: 9786208419547
Cantidad disponible: 2 disponibles
Librería: Majestic Books, Hounslow, Reino Unido
Condición: New. Print on Demand. Nº de ref. del artículo: 409623648
Cantidad disponible: 4 disponibles
Librería: Biblios, Frankfurt am main, HESSE, Alemania
Condición: New. PRINT ON DEMAND. Nº de ref. del artículo: 18404612021
Cantidad disponible: 4 disponibles
Librería: AussieBookSeller, Truganina, VIC, Australia
Paperback. Condición: 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. Nº de ref. del artículo: 9786208419547
Cantidad disponible: 1 disponibles
Librería: CitiRetail, Stevenage, Reino Unido
Paperback. Condición: 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. Nº de ref. del artículo: 9786208419547
Cantidad disponible: 1 disponibles