How Airplanes Stay Up—and Why Wings Stall
AXIOM & GEAR
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How Airplanes Stay Up—and Why Wings Stall
72 просмотра · 6 дн. назад
AXIOM & GEAR
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72 просмотра · 6 дн. назад
What actually holds an airplane up—and why can asking a wing for more eventually give us less?
Follow one aircraft into its wing. We connect pressure and the air's momentum, make the lift equation useful, separate angle of attack from the horizon, and compare an ideal calculation with real wind-tunnel stall measurements. Five questions let you try the reasoning before the explanation.
CHAPTERS
00:00 The same air, a different wing
01:05 Which way is lift?
02:30 Small pushes, one force
04:00 The air has no reunion rule
05:24 An equation that earns its place
07:14 The angle the air actually sees
08:48 Ask a real wind tunnel
10:21 When the smooth picture breaks
12:00 What the engine contributes
13:03 The air behind the whole wing
14:28 A lesson from a small wind tunnel
15:08 Back to the airplane
The smooth-flow visualization is an original ideal Joukowski calculation: steady, two-dimensional, incompressible and inviscid. It cannot predict boundary-layer separation or stall. The measured curve is a separate NACA 0012 experiment: Mach 0.15, Reynolds number 5.95 million, No.80-W transition strips at 5% chord on both surfaces. Separation and wingtip-wake animations are clearly labeled schematics. No universal stall angle is implied.
SOURCES AND FURTHER READING
NASA — Bernoulli and Newton: https://www1.grc.nasa.gov/beginners-g...
NASA — Lift equation: https://www1.grc.nasa.gov/beginners-g...
Ladson (1988), NASA TM4074: https://ntrs.nasa.gov/citations/19880...
NASA TMR — original measured coefficient table: https://tmbwg.github.io/turbmodels/NA...
FAA — Pilot's Handbook of Aeronautical Knowledge, Chapter 5: https://www.faa.gov/sites/faa.gov/fil...
NASA — Wright wind-tunnel measurements: https://www.grc.nasa.gov/www/k-12/air...
1903 first-flight photograph: Wright brothers/John T. Daniels, Library of Congress, Prints and Photographs Division, LC-W86-35; https://www.loc.gov/item/00652085/ . Item advisory: no known restriction on publication. No institutional endorsement is implied.
Original explanation, animation and contextual sound: AXIOM & GEAR.
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