$$\displaystyle V=S_{0}RMN\quad\text{intér}\qquad V=R_{0}SMN\quad\text{extér.}$$
	$$\displaystyle V_{1}=S^{0}_{1}R_{1}M_{1}N_{1};\quad\int V\frac{dV_{1}}{dn}d\omega=0;\int RMNR^{\prime}_{1}M_{1}N_{1}\frac{d\rho}{dn}d\omega=0$$
	$$\displaystyle\frac{d\rho}{dn}=\frac{1}{\alpha}=\frac{OP}{\rho}=\frac{\sqrt{\mu^{2}-\nu^{2}}A}{Q};\quad OP=\frac{\sqrt{\mu^{2}-\nu^{2}}\rho A}{Q}=\frac{\sqrt{(\rho^{2}-a^{2})(\rho^{2}-b^{2})(\rho^{2}-c^{2})}}{\sqrt{(\rho^{2}-\mu^{2})(\rho^{2}-\nu^{2})}}$$
	$$\displaystyle\ell=\frac{1}{\sqrt{(\rho^{2}-\mu^{2})(\rho^{2}-\nu^{2})}}=\frac{OP}{\sqrt{(\rho^{2}-a^{2})(\rho^{2}-b^{2})(\rho^{2}-c^{2})}};\quad\frac{d\rho}{dn}=\ell iA$$
	$$\displaystyle\int\ell MNM_{1}N_{1}d\omega=0;\quad F=\sum K_{i}M_{i}N_{i};\quad\int\ell M_{j}N_{j}Fd\omega$$
	$$\displaystyle=\sum K_{i}\int\ell M_{i}N_{i}M_{j}N_{j}d\omega=K_{j}\int\ell M^{2}_{j}N^{2}_{j}d\omega$$

$$F=\sum KMN;\quad\text{int.}\;V=\sum\frac{KRMN}{R_{0}};\quad\text{ext.}\;V=\sum\frac{KSMN}{S_{0}}$$

	$$\displaystyle\frac{\zeta}{\ell}=\sum C\cdot MN;\quad\text{int.}\;V=\sum\frac{KRMN}{R_{0}};\quad\text{ext.}\;V=\sum\frac{KSMN}{S_{0}}$$
	$$\displaystyle\frac{dV}{dn}=\sum\ell iA\frac{KR^{\prime}\cdot MN}{R}\quad\text{int.}\qquad\text{ext.}\quad\sum\frac{\ell iAKS^{\prime}\cdot MN}{S}$$
	$$\displaystyle\ell iAK\left(\frac{R^{\prime}}{R}-{S^{\prime}}{S}\right)=4\pi\ell C$$
	$$\displaystyle A(R^{\prime}S-S^{\prime}R)=-i(2n+1);\quad\frac{+K(2n+1)}{RS}=4\pi C$$
	$$\displaystyle K=+\frac{4\pi CRS}{2n+1};\quad V=+\sum\frac{4\pi CS_{0}RMN}{2n+1}$$

	$$\displaystyle\text{rapport}\;\varepsilon;\quad\zeta=PP_{1}=\varepsilon OP=$$
	$$\displaystyle\frac{\varepsilon\ell}{\sqrt{(\rho^{2}-a^{2})(\rho^{2}-b^{2})(\rho^{2}-c^{2})}}=\frac{4}{3}\pi\frac{\varepsilon\ell}{T};\;T\;\text{vol. ellips.}$$
	$$\displaystyle V=\frac{(4\pi)^{2}}{3}\frac{\varepsilon}{T}S\quad\text{ou}\quad R=1.$$

$$\varepsilon\frac{dV}{dx}$$

	$$\displaystyle MM_{1}=\varepsilon$$
	$$\displaystyle MP=\zeta\qquad\text{angle}\;PMM_{1}=\theta.$$
	$$\displaystyle\zeta=\varepsilon\cos\theta.$$
	$$\displaystyle M\;(\rho,\mu,\nu,)\;Q\;\rho+d\rho,\mu,\nu$$
	$$\displaystyle x,y,z\qquad x+dx\;\text{etc.}\quad R=\sqrt{\rho^{2}-a^{2}}$$

	$$\displaystyle\cos\theta=\frac{dx}{d\rho}\frac{d\rho}{dn}=\frac{x\rho}{\sqrt{\rho^{2}-a^{2}}}\frac{d\rho}{dn};\quad RMN=x\sqrt{(a^{2}-b^{2})(a^{2}-c^{2})}$$
	$$\displaystyle\cos\theta=\frac{x\rho}{\sqrt{\rho^{2}-a^{2}}}\frac{d\rho}{dn}=\ell iA\frac{x\rho}{\sqrt{\rho^{2}-a^{2}}}=\ell x\sqrt{(\rho^{2}-b^{2})(\rho^{2}-c^{2})}$$
	$$\displaystyle\zeta=\ell\varepsilon RMN\sqrt{\frac{(\rho^{2}-b^{2})(\rho^{2}-c^{2})}{(a^{2}-b^{2})(a^{2}-c^{2})}}=\frac{\ell\varepsilon T}{\left(\frac{4}{3}\pi\right)}\frac{MN}{\sqrt{(a^{2}-b^{2})(a^{2}-c^{2})}}$$
	$$\displaystyle\frac{dV}{dx}=\sqrt{(\rho^{2}-b^{2})(\rho^{2}-c^{2})}\frac{4}{3}\pi\frac{RMNS_{0}}{\sqrt{(a^{2}-b^{2})(a^{2}-c^{2})}}$$

	$$\displaystyle\triangle u=0,\quad S:u=Q;\quad M-Q=\varpi;\quad S:\varpi=0,\quad\triangle\varpi=-\triangle Q=f$$
	$$\displaystyle\int\left[\sum\left(\frac{d\varpi}{dx}\right)^{2}+2\varpi f\right]d\tau=J;\quad\int\left[\sum\frac{d\varpi}{dx}\frac{d\delta\varpi}{dx}+f\delta\varpi\right]d\tau=0$$
	$$\displaystyle\int\delta\varpi\frac{d\varpi}{dn}d\omega-\int\delta\varpi(\triangle\varpi-f)d\tau=0;\quad\varpi=\sum A_{i}\psi_{i}$$

1° $\psi$ continue sur $R$ et sur son bord ainsi que ses dérivées principales. $m,n,p=0,1,2$
2° Sur le bord $\psi=0$; $\zeta$
3° $\cdots$ $\zeta$ représ. par séries, toutes les fois que $\zeta$ continue ainsi que ses dérivées princip.
4° $\zeta_{m}=0$ entraîne $A_{1}=A_{2}=\cdots=A_{m}=0$ si $\zeta_{m}=\sum A_{i}\psi_{i}$

On fera $\psi_{i}=F\begin{smallmatrix}\sin\\ \cos\end{smallmatrix}mx\begin{smallmatrix}\sin\\ \cos\end{smallmatrix}ny\begin{smallmatrix}\sin\\ \cos\end{smallmatrix}pz$; $F=0$.

	$$\displaystyle\int\left(\varpi_{m}\triangle\zeta_{m}-f\zeta_{m}\right)d\tau=0;\quad\int\left[\sum\frac{d\varpi_{m}}{dx}\frac{d\zeta_{m}}{dx}+f\zeta_{m}\right]d\tau=0$$
	$$\displaystyle\int\varpi_{m}\frac{d\zeta_{m}}{dn}d\omega-\int\left(\varpi_{m}\triangle\zeta_{m}-f\zeta_{m}\right)d\tau=0$$

	$\displaystyle J_{p}$	$\displaystyle=\int\left[\sum\left(\frac{d\varpi_{p}}{dx}\right)^{2}+2f\varpi_{p}\right]d\tau\qquad(1)\qquad pq$
	$\displaystyle J_{q}$	$\displaystyle=\int\left[\sum\left(\frac{d\varpi_{q}}{dx}\right)^{2}+2f\varpi_{q}\right]d\tau\qquad(-1)$
	$\displaystyle Q$	$\displaystyle=\int\left[\sum\frac{d\varpi_{q}}{dx}\frac{d(\varpi_{q}-\varpi_{p}}{dx}+f(\varpi_{q}-\varpi_{p})\right]d\tau\qquad(2)$

$$J_{p}-J_{q}=\int\sum\left[\frac{d(\varpi_{q}-\varpi_{p}}{dx}\right]^{2}d\tau$$

AD 3p. Collection particulière, Paris 75017.

Time-stamp: " 5.05.2019 01:04"