Pressure fields change on both surfaces, with the upper low-pressure zone doing most of the work.
Parasite drag is the resistance caused by moving a solid object through a fluid medium, unrelated to the production of lift. It divides into three types:
Bernoulli's principle states that an increase in the speed of a fluid occurs simultaneously with a decrease in static pressure. While this relationship is correct, popular explanations use it as a primary cause rather than a secondary effect. They fail to explain why the air speeds up over the top of the wing in the first place. The Real Physics of Lift Generation
Why does the air follow the curved upper surface of a wing instead of just flying off in a straight line?
Doug McLean’s Understanding Aerodynamics: Arguing from the Real Physics serves as a vital correction to the oversimplified narratives that have dominated aerodynamic instruction. By stripping away the math-first reliance on abstract circulation and focusing on the causal chain of events—viscosity enforcing flow attachment, geometry dictating pressure gradients, and pressure fields imparting momentum—this paper demonstrates that lift is a unified physical phenomenon. The "real physics" approach restores the primacy of physical intuition, ensuring that the equations used to predict flight are grounded in the reality of how fluids actually move. understanding aerodynamics arguing from the real physics pdf
Limitations force inclusion of viscosity near solid surfaces.
A fundamental law of fluid mechanics dictates that whenever a fluid flows along a curved path, a pressure gradient perpendicular to the flow direction must exist.
This public link is valid for 7 days and shares a thread, including any personal information you added. This link or copies made by others cannot be deleted. If you share with third parties, their policies apply. Can’t copy the link right now. Try again later.
As McLean’s own book demonstrates, physical understanding can be conveyed without drowning the reader in equations. A “real physics” PDF should include the essential equations (e.g., Bernoulli’s equation, the Kutta–Joukowski theorem, the boundary‑layer momentum integral equation) but should always follow each equation with a plain‑English interpretation of what it means physically. . Pressure fields change on both surfaces, with the
In the real world, fluids have viscosity. As air flows over a wing, friction creates a thin layer of slow-moving air directly against the surface called the . This boundary layer prevents the flow from cleanly wrapping around the trailing edge without separation, altering the effective shape of the airfoil. Circulation and the Kutta Condition
McLean argues that lift cannot be explained by a single, isolated physical law. Instead, lift is the result of a cause-and-effect loop where pressure fields, velocity fields, and momentum conservation act simultaneously. The Cause-and-Effect Loop
Air follows the wing shape due to the "Coandă Effect" magic.
While Newton's laws describe the global force balance, Bernoulli's principle describes the localized mechanics within the fluid field. Bernoulli's principle states that within a steady, horizontal flow of fluid, an increase in fluid velocity occurs simultaneously with a decrease in static pressure. While this relationship is correct, popular explanations use
Air cannot simply vanish. If air flows through a narrower section (like over a curved wing), it must accelerate to get the same amount of mass through the area in the same amount of time [1].
This is elegant, intuitive, and utterly false. There is no law of nature compelling two parcels of air that split at the leading edge to reunite at the back. In fact, wind tunnel experiments show the air over the top reaches the trailing edge well before the air underneath. The equal transit time myth survives only because it fits a pre-digested narrative. Real physics demands more.
According to the , the lift per unit span ( L′cap L prime ) is directly proportional to the fluid density ( ), the free-stream velocity ( V∞cap V sub infinity end-sub ), and the circulation ( Γcap gamma
Explain lift while tracking assumptions: thin-airfoil approximations, small-angle linearization, or the necessity of viscous effects to enforce Kutta condition.