Shufeng Zhang,
Please dig up Sakurai QM and review the Density Matrix formulation of QM/Thermo. Integrals are just that...they help show conservat... [more]
Shufeng Zhang,
Please dig up Sakurai QM and review the Density Matrix formulation of QM/Thermo. Integrals are just that...they help show conservation and general stuff like Gauss's law, BUT not-for-an-instant do they address the QM foundations of thermo which enables the prediction of properties of metals at low temperature. I guess I'll have to post a paper showing this?
Shufeng,
The world of thermo defined by the integrals is not necessarily the best place to start when it comes to reality. We know from a simple syst... [more]
Shufeng,
The world of thermo defined by the integrals is not necessarily the best place to start when it comes to reality. We know from a simple system composed of a piston and two volumes that the effects of entropy can be witnessed physically. Also I'd like to recommend Sakurai - Modern Quantum Mechanics. In the course of about 4 pages he links the DM to the standard thermo concepts. Entropy can be easily distilled from the DM...and for everyone else "it's not disorder but increased multiplicity."
Shufeng,
The world of thermo defined by the integrals is not necessarily the best place to start when it comes to reality. We know from a simple s... [more]
Shufeng,
The world of thermo defined by the integrals is not necessarily the best place to start when it comes to reality. We know from a simple system composed of a piston and two volumes that the effects of entropy can be witnessed physically. Also I'd like to recommend Sakurai - Modern Quantum Mechanics. In the course of about 4 pages he links the DM to the standard thermo concepts. Entropy can be easily distilled from the DM...and for everyone else "it's not disorder but increased multiplicity."
[show abstract][hide abstract] ABSTRACT: Mars atmospheric and global surface investigations will benefit greatly from the aerial mobility of flying platforms. "First Flyers" for Mars exploration includes terrain explorers and parasail-delivered landers. Future manned missions would also benefit from autonomous flight operations, which could greatly reduce the risks associated with landing site selection. Two concepts were designed for launch on a Delta II booster and are evaluated in this report: an improved mid-weight version of the early large-span flyer (JPLDSI, 1978) and a parasail delivery system. In addition to classical design practices, a systems engineering, risk reduction approach is developed which delineates the necessary technology developments to achieve desired performance and mission success.