Abstract: A gas turbine engine is provided. The gas turbine engine includes: a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order, the compressor section having a high pressure compressor defining a high pressure compressor exit area (AHPCExit) in square inches; wherein the gas turbine engine defines a redline exhaust gas temperature (EGT) in degrees Celsius, a total sea level static thrust output (FnTotal) in pounds, and a corrected specific thrust, wherein the corrected specific thrust is greater than or equal to 42 and less than or equal to 90, the corrected specific determined as follows: FnTotal×EGT/(AHPCExit2×1000).

Abstract: A computer system comprising a processor for executing program instructions and a memory coupled to the processor for storing the program instructions, the programming instructions comprising: enter intake data on a patient; entering symptoms the patient is experiencing and services performed on the patient, wherein all symptom and services listed in the program instructions are assigned a numeric number based on severity of the symptom and service; calculating total value of all numeric values of symptoms patient is experiencing and services performed on the patient; and making a recommendation to one of continue hospital stay or discharge of the patient.

Abstract: A computer system comprising a processor for executing program instructions and a memory coupled to the processor for storing the program instructions, the programming instructions comprising: enter intake data on a patient; entering symptoms the patient is experiencing and services performed on the patient, wherein all symptom and services listed in the program instructions are assigned a numeric number based on severity of the symptom and service; calculating total value of all numeric values of symptoms patient is experiencing and services performed on the patient; and making a recommendation to one of continue hospital stay or discharge of the patient.