4 ms·
For those curious about the unusual overwing engine pods, Wikipedia says: "The HondaJet’s overwing engine mount configuration was designed to maximize cabin sp
by perilunar 8y ago
For those curious about the unusual overwing engine pods, Wikipedia says:
"The HondaJet’s overwing engine mount configuration was designed to maximize cabin space,[5] and achieve lower wave drag at a high Mach number."
https://en.wikipedia.org/wiki/Honda_HA-420_HondaJet#Design https://en.wikipedia.org/wiki/Honda_HA-420_HondaJet#Design
The source document has more discussion of the issues involved:
http://www.hondajet.com/Content/pdf/FlightInternational_CoverStory.pdf http://www.hondajet.com/Content/pdf/FlightInternational_Cove...
- pritambaral 8y agoThe source document is especially helpful. The overwing engine configuration is unusual because it has been an industry-accepted fact that flow interference (specifically, the conversion of the flow from laminar to turbulent) from the wing as the angle of attack increased beyond a few degrees — which happens during take-off, climb, and landing with wing-aerodynamic braking — would have significant-to-catastrophic effects on the engine's intake. Honda says they managed to find a sweet spot amidst the interference, using computational analysis and wind-tunnel testing. Computational analysis of turbulent flows is much more difficult than laminar flows, and wind-tunnel testing has been traditionally favoured over computational analysis for this reason. Honda also says they made their own airfoil and made the upper-skin extra smooth to keep the flow more laminar between the wing and the engine. This is impressive engineering. EDIT: Just noticed, the document claims the wing had to be made of metal instead of composites " to maintain the contour required for laminar flow".
- cup-of-tea 8y agoIs it normal to talk about a "high Mach number" for a subsonic aircraft?
- mseebach 8y agoYes. At high (sub sonic) speed and high altitude, you get close enough to the speed of sound that this starts to matter a lot. https://aviation.stackexchange.com/questions/35408/what-is-the-reason-for-changing-the-speed-reference-ias-or-mach-number-with-al https://aviation.stackexchange.com/questions/35408/what-is-t...
- sandworm101 8y agoMach is the better reference. If you quote standard speeds you get into the whole ground/indicated/actual speed/alt issue. Your numbers will always sound wrong to someone. Mach avoids the issue.