Abstract: The present invention relates to a fermented herbal health drink, comprising extract from plant Andrographis, extract from barley, wheat, and/or fruit and ethanol concentration ranging between 3 to 13% in the total health drink and optionally extract from plant Tinospora and other additives, said drink not containing hops and still having characteristic taste of a beer with no adverse effect and contributing to several medicinal properties comprising anti-oxidant, nervine relaxant, cholerectic, cardio-tonic, diurectic, digestive and immunomodulant, and a method of producing the herbal health drink, preferably a method of introducing bitterness into said health drink and using the same as a beer or to produce beer with said medicinal properties.

Abstract: The present invention relates to a fermented herbal health drink, comprising extract from plant Andrographis, extract from barley, wheat, and/or fruit and ethanol concentration ranging between 3 to 13% in the total health drink and optionally extract from plant Tinospora and other additives, said drink not containing hops and still having characteristic taste of a beer with no adverse effect and contributing to several medicinal properties comprising anti-oxidant, nervine relaxant, cholerectic, cardio-tonic, diurectic, digestive and immunomodulant, and a method of producing the herbal health drink, preferably a method of introducing bitterness into said health drink and using the same as a beer or to produce beer with said medicinal properties.

Abstract: The present invention is embodied in an apparatus and method for generating fatigue spectra on a chosen aircraft for which a Finite element model is available and for which a library of external load summations at key interfaces and key fundamental parameters are available from an aeroelastic analysis. The fatigue spectra generation system of the present invention represents a profile of stresses endured by the aircraft due to numerous events, such as ground and maneuver events, occurring during the life of the aircraft. The system calculates a total stress based on load and unit conditions associated with outside events by factoring up the unit conditions to derive individual stresses for each event and by summing all unit conditions.