diff --git a/_index.db b/_index.db index d1b48162d..86f68b526 100644 Binary files a/_index.db and b/_index.db differ diff --git a/data/en.wikipedia.org/wiki/IEEE_Robert_N._Noyce_Medal-0.md b/data/en.wikipedia.org/wiki/IEEE_Robert_N._Noyce_Medal-0.md new file mode 100644 index 000000000..bf1f48958 --- /dev/null +++ b/data/en.wikipedia.org/wiki/IEEE_Robert_N._Noyce_Medal-0.md @@ -0,0 +1,23 @@ +--- +title: "IEEE Robert N. Noyce Medal" +chunk: 1/1 +source: "https://en.wikipedia.org/wiki/IEEE_Robert_N._Noyce_Medal" +category: "reference" +tags: "science, encyclopedia" +date_saved: "2026-05-05T11:53:10.928167+00:00" +instance: "kb-cron" +--- + +The IEEE Robert N. Noyce Medal is a science award presented by the IEEE for outstanding contributions to the microelectronics industry. It is given to individuals who have demonstrated contributions in multiple areas including technology development, business development, industry leadership, development of technology policy, and standards development. The medal is named in honour of Robert N. Noyce, the co-founder of Intel Corporation. He was also renowned for his 1959 invention of the integrated circuit. The medal is funded by Intel Corporation and was first awarded in 2000. + + +== Recipients == +Source: + + +== References == + + +== External links == +IEEE Robert N. Noyce Medal, Institute of Electrical and Electronics Engineers +Recipients of the Robert N. Noyce Medal, Institute of Electrical and Electronics Engineers \ No newline at end of file diff --git a/data/en.wikipedia.org/wiki/Orders_of_magnitude_(torque)-0.md b/data/en.wikipedia.org/wiki/Orders_of_magnitude_(torque)-0.md new file mode 100644 index 000000000..cba4e47cf --- /dev/null +++ b/data/en.wikipedia.org/wiki/Orders_of_magnitude_(torque)-0.md @@ -0,0 +1,17 @@ +--- +title: "Orders of magnitude (torque)" +chunk: 1/1 +source: "https://en.wikipedia.org/wiki/Orders_of_magnitude_(torque)" +category: "reference" +tags: "science, encyclopedia" +date_saved: "2026-05-05T11:52:07.196535+00:00" +instance: "kb-cron" +--- + +The following are examples of orders of magnitude for torque. + + +== Examples == + + +== References == \ No newline at end of file diff --git a/data/en.wikipedia.org/wiki/Oswald_efficiency_number-0.md b/data/en.wikipedia.org/wiki/Oswald_efficiency_number-0.md new file mode 100644 index 000000000..5368898b3 --- /dev/null +++ b/data/en.wikipedia.org/wiki/Oswald_efficiency_number-0.md @@ -0,0 +1,329 @@ +--- +title: "Oswald efficiency number" +chunk: 1/1 +source: "https://en.wikipedia.org/wiki/Oswald_efficiency_number" +category: "reference" +tags: "science, encyclopedia" +date_saved: "2026-05-05T11:52:08.344773+00:00" +instance: "kb-cron" +--- + +The Oswald efficiency, similar to the span efficiency, is a correction factor that represents the change in drag with lift of a three-dimensional wing or airplane, as compared with an ideal wing having the same aspect ratio and an elliptical lift distribution. + + +== Definition == +The Oswald efficiency is defined for the cases where the overall coefficient of drag of the wing or airplane has a constant+quadratic dependence on the aircraft lift coefficient + + + + + + C + + D + + + = + + C + + + D + + 0 + + + + + + + + + + ( + + C + + L + + + + ) + + 2 + + + + + π + + e + + 0 + + + A + R + + + + + + {\displaystyle C_{D}=C_{D_{0}}+{\frac {(C_{L})^{2}}{\pi e_{0}AR}}} + + +where + +For conventional fixed-wing aircraft with moderate aspect ratio and sweep, Oswald efficiency number with wing flaps retracted is typically between 0.7 and 0.85. At supersonic speeds, Oswald efficiency number decreases substantially. For example, at Mach 1.2 Oswald efficiency number is likely to be between 0.3 and 0.5. + + +== Comparison with span efficiency factor == +It is frequently assumed that Oswald efficiency number is the same as the span efficiency factor which appears in lifting-line theory, and in fact the same symbol e is typically used for both. But this assumes that the profile drag coefficient is independent of + + + + + C + + L + + + + + {\displaystyle C_{L}} + +, which is certainly not true in general. Assuming that the profile drag itself has a constant+quadratic dependence on + + + + + C + + L + + + + + {\displaystyle C_{L}} + +, +an alternative drag coefficient breakdown can be given by + + + + + + C + + D + + + = + + c + + + d + + 0 + + + + + + + + c + + + d + + 2 + + + + + ( + + C + + L + + + + ) + + 2 + + + + + + + + ( + + C + + L + + + + ) + + 2 + + + + + π + e + A + R + + + + + + {\displaystyle C_{D}=c_{d_{0}}+c_{d_{2}}(C_{L})^{2}+{\frac {(C_{L})^{2}}{\pi eAR}}} + + +where + +Equating the two + + + + + C + + D + + + + + {\displaystyle C_{D}} + + expressions gives the relation between the Oswald efficiency number e0 and the lifting-line span efficiency e. + + + + + + C + + + D + + 0 + + + + + = + + c + + + d + + 0 + + + + + + + {\displaystyle C_{D_{0}}=c_{d_{0}}} + + + + + + + + 1 + + e + + 0 + + + + + = + + + 1 + e + + + + + π + A + R + + c + + + d + + 2 + + + + + + + {\displaystyle {\frac {1}{e_{0}}}={\frac {1}{e}}+\pi ARc_{d_{2}}} + + +For the typical situation + + + + + c + + + d + + 2 + + + + + > + 0 + + + {\displaystyle c_{d_{2}}>0} + +, we have + + + + + e + + 0 + + + < + e + + + {\displaystyle e_{0}