Area rule
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The Whitcomb area rule, also called the transonic area rule, is a design technique used to reduce an aircraft's drag at transonic and supersonic speeds, particularly between Mach 0.75 and 1.2.
- See also: Wikipedia
- Related: Anti-shock body, Sonic boom, Sound barrier
Aerospaceweb.org: Area rule explained Aerospaceweb.org: Area rule explained www.aerospaceweb.org/question/aerodynamics/q0104.shtml - Web |
Aerospaceweb.org: Whitcomb Area Rule and Küchemann... Aerospaceweb.org: Whitcomb Area Rule and Küchemann Carrots www.aerospaceweb.org/question/aerodynamics/q0240.shtml - Web |
DGLR document DGLR document www.dglr.de/.../Kapitel2_3_4.pdf - Web |
Gallery for «Area rule»
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German patent search system - look for Patent DE 9... German patent search system - look for Patent DE 932410 filed March 21, 1944 www.depatisnet.de - Web |
NASA 2004: Overuse increases drag but still reduce... NASA 2004: Overuse increases drag but still reduces boom heard on the ground www.nasa.gov/missions/research/sonic_booms.html - Web |
See Image 4 for an extreme example: fuselage befor... See Image 4 for an extreme example: fuselage before wing www.pbs.org/wgbh/nova/concorde/shock.html - Web |
The Whitcomb Area Rule: NACA Aerodynamics Research... The Whitcomb Area Rule: NACA Aerodynamics Research and Innovation history.nasa.gov/SP-4219/Chapter5.html - Web |
Contemporary reporting and explanation of area rul... Contemporary reporting and explanation of area rule www.flightglobal.com/pdfarchive/view/1955/1955%20-%201648.html - Web |