سبد اکانت پایگاه های اطلاعاتی 
سبد منابع اطلاعاتی 
NASA-CR-165843 : Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles
سازمان: NASA - National Aeronautics and Space Administration (NASA)
کلید واژه: AIRCRAFT , ANALYSIS , COMPUTER , CRUISE , DESIGN , EDGE , ESTIMATES , FLAPS , LEADING , PROGRAMS , RESEARCH , SUPERSONIC , THRUST , WINGS
سال: 1982
زبان: English
قیمت: 290000 تومان
A study of low speed leading-edge flap design for supersonic cruise vehicle was conducted. Wings with flaps were analyzed with the aid of a newly developed subsonic wing program which provides estimates of attainable leading-edge thrust. Results indicate that the thrust actually attainable can have a significant influence on the design and that the resultant flaps can be smaller and simpler than those resulting from more conventional approaches.
NASA-CR-165843 : Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles
سازمان: NASA - National Aeronautics and Space Administration (NASA)
کلید واژه: AIRCRAFT , ANALYSIS , COMPUTER , CRUISE , DESIGN , EDGE , ESTIMATES , FLAPS , LEADING , PROGRAMS , RESEARCH , SUPERSONIC , THRUST , WINGS
سال: 1982
زبان: English
قیمت: 290000 تومان
A study of low speed leading-edge flap design for supersonic cruise vehicle was conducted. Wings with flaps were analyzed with the aid of a newly developed subsonic wing program which provides estimates of attainable leading-edge thrust. Results indicate that the thrust actually attainable can have a significant influence on the design and that the resultant flaps can be smaller and simpler than those resulting from more conventional approaches.
