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The Whitcomb area rule, named after a US National Advisory Committee for Aeronautics (NACA) engineer Richard Whitcomb and also called the transonic area rule, is a design procedure used to reduce an aircraft's drag at transonic speeds which occur between about Mach 0.75 and 1.2. For supersonic speeds a different procedure called the supersonic area rule…
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area rule drag aircraft speed supersonic mach fuselage transonic wing whitcomb also speeds body naca flow wave shape design rear
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| the Bombardier Global Express | instance of | and rear fuselage thinning on business jets with rear engines | 0.80 | text |
| Area rule | has application | The | 0.60 | section |
| Area rule | has application | German | 0.60 | section |
| Area rule | has application | Junkers Ju-287 | 0.60 | section |
| Area rule | has application | Other | 0.60 | section |
| Area rule | has application | When | 0.60 | section |
| Area rule | has application | Whitcomb | 0.60 | section |
| Area rule | has application | US | 0.60 | section |
| Area rule | has application | Convair | 0.60 | section |
| Area rule | has application | Grumman | 0.60 | section |
| Area rule | has application | Whitcomb's | 0.60 | section |
| Area rule | has application | Grumman F-11 Tiger | 0.60 | section |
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