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A common-origin pressure-tap position error shifts several inferred tap positions together relative to a fixed physical reference. It is a shared contribution to correlated position errors of pressure taps, not an independent placement error for every hole. Whether it affects a pressure-derived load depends on which references are held fixed.

For dimensionless chord coordinate $\xi$, suppose the uncertain displacement is the same scalar $e$ for every tap. A first-order Taylor expansion of the pressure coefficient gives $\delta C_{p,i}\simeq C_p^{\prime }({\xi }_i)e$. For a reconstruction $Q={\sum }_i{w}_i{C}_{p,i}$ with fixed quadrature weights,The position covariance matrix is $u_e^{2}11^T$, a rank-one matrix. Squaring each tap's contribution before adding would discard the shared covariances. The covariance terms belong in the general propagation of uncertainty.^[ref]

An original locally linear example takes eight equal weights $w_i=1/8$, equal local slopes $C_p^{\prime }=20$ and $u_e=0.002$. The reconstructed coefficient has standard uncertainty $u_Q=0.040$. Incorrect independence would give $0.040/\sqrt{8}\approx 0.0141$. If a two-dimensional load per span is $L^{\prime }=qcQ$ with stipulated dynamic pressure $q=500$ Pa and airfoil chord $c=0.20$ m, these become $4.0$ and $1.41$ N/m. The chosen slopes describe a sensitivity model, not measured airfoil data.

Opposite-signed sensitivities can cancel the shared contribution. Conversely, repeating coordinate readings without independently checking the misplaced datum cannot average away its fixed error. A proposed test measures an independent reference mark and deliberately translates the assumed origin in the reconstruction, comparing the observed load sensitivity with the derivative above. If moving coordinates also changes the integration weights, those additional derivatives must be included.

Pressure-tap datum cancellation is a different situation. When the tap, leading edge and trailing edge are all expressed through the same affine map $u=a+bx$, with $b>0$,The common origin and scale cancel exactly. Merely translating a shared coordinate system causes no physical tap misregistration. Affine pressure-tap coordinate calibration must therefore state whether the datum is shared or independently fixed before assigning a common-origin uncertainty.

A pressure-tap position error assigns a measured surface pressure to the wrong point on an airfoil. This differs from a pressure transducer's pressure-reading error: an accurate instrument can faithfully measure the pressure at a misplaced or incorrectly labeled hole. A steep spatial pressure gradient makes a small location error important.

Let $\xi =x/c$ be the nominal chord coordinate and let the actual pressure tapping lie at $\xi +\epsilon$. For a differentiable pressure coefficient profile,If the derivative is bounded by $K$ throughout the interval between the two positions, the mean value theorem gives the rigorous bound $|\delta C_p|\le K|\epsilon |$. Knowing only an endpoint slope does not establish that bound across an unresolved peak.

In an original local example, take $c=0.20\mathrm{m}$, a physical position error $\delta x=0.40\mathrm{mm}$, and a profile locally linear with $C_p^{\prime }=20$. Then $\epsilon =0.002$ and $\delta C_p=0.040$. At dynamic pressure $q=500\mathrm{Pa}$, the corresponding pressure difference is $q\delta C_p=20\mathrm{Pa}$. These are stipulated values illustrating sensitivity, not measurements of a particular airfoil.

For fixed quadrature weights $\mathbf{w}$ and small errors in several tap positions, put $J=\mathrm{diag}(C_p^{\prime }({\xi }_i))$. If ${\Sigma }_{\xi }$ is their position-error covariance matrix, the first-order variance contribution to a reconstructed coefficient isThis formula retains correlated position errors of pressure taps, including a shared coordinate-origin error. It holds the reconstruction weights and surface geometry fixed; uncertainty in those also needs accounting when geometry is inferred from the same coordinates.

Pressure-tap position calibration measures the actual hole coordinates and their reference origin, alongside pressure-channel calibration. Robert M. Pinkerton's distributed-pressure experiment used 54 orifices on an airfoil model to compare a measured distribution with potential flow predictions.^[ref] Such a comparison tests both where a feature occurs and how large it is; pressure-only calibration cannot fix a displaced coordinate.