Global Information Lookup Global Information

Busemann biplane information


Busemann's original biplane operating at its design point

The Busemann biplane is a theoretical aircraft configuration invented by Adolf Busemann, which avoids the formation of N-type shock waves and thus does not create a sonic boom or the associated wave drag. However in its original form it does not generate lift either. A Busemann biplane concept, which provides adequate lift, and which can reduce the wave intensity and drag but not eliminate them, has been studied for a "boomless" supersonic transport.

and 6 Related for: Busemann biplane information

Request time (Page generated in 0.7416 seconds.)

Busemann biplane

Last Update:

The Busemann biplane is a theoretical aircraft configuration invented by Adolf Busemann, which avoids the formation of N-type shock waves and thus does...

Word Count : 799

Adolf Busemann

Last Update:

Paperclip, invented the shockwave-free supersonic Busemann biplane. Born in Lübeck, Germany, Busemann attended the Technical University of Braunschweig...

Word Count : 909

Busemann

Last Update:

the author of Busemann's theorem Busemann biplane Busemann's theorem Busemann function This page lists people with the surname Busemann. If an internal...

Word Count : 90

Wing configuration

Last Update:

smaller upper wing. The Fiat CR.1 was in production for many years. Busemann biplane: a theoretical supersonic wing configuration, in which shock waves...

Word Count : 5548

Sonic boom

Last Update:

theoretical designs do not appear to create sonic booms at all, such as the Busemann biplane. However, creating a shockwave is inescapable if it generates aerodynamic...

Word Count : 3633

Swept wing

Last Update:

first investigated in Germany as early as 1935 by Albert Betz and Adolph Busemann, finding application just before the end of the Second World War. It has...

Word Count : 8233

PDF Search Engine © AllGlobal.net