Efficient computation of the complex error function
Complex error function computation using approximation method with single algorithm
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Complex error function computation using approximation method with single algorithm
Multichannel apparatus produces or simulates a complex curve which can be viewed on an oscilloscope display surface and can be adjusted to match an original complex experimentally produced curve.
Saturn I /SA-9/ launch vehicle and Launch Complex 37 pad accessories - umbilical tower swing arms, short cable masts, fuel and liquid oxygen masts, and holddown arms
Liquid hydrogen system for Saturn 9 vehicle propulsion
Computation of complex error function
A survey and comparison of some computational methods and algorithms for gamma and log-gamma functions of complex arguments are presented. Methods and algorithms reported include Chebyshev approximations, Pade expansion and Stirling's asymptotic series. The comparison leads to the conclusion that Algorithm 421 published in the Communications of ACM by H. Kuki is the best program either for individual application or for the inclusion in subroutine libraries.
Saturn launch vehicle and launch complex functional description - RP-1 fuel system, finding numbers, and schematics
A generalized wall function was proposed by Shih et al., (1999). It accounts the effect of pressure gradients on the flow near the wall. Theory shows that the effect of pressure gradients on the flow in the inertial sublayer is very significant and the standard wall function should be replaced by a generalized wall function. Since the theory is also valid for boundary layer flows toward separation, the generalized wall function may be applied to complex turbulent flows with acceleration, deceleration, separation and recirculation. This paper is to verify the generalized wall function with numerical simulations for boundary layer flows with various adverse and favorable pressure gradients, including flows about to separate. Furthermore, a general procedure of implementation of the generalized wall function for National Combustion Code (NCC) is described, it can be applied to both structured and unstructured CFD codes.
Saturn I /SA-10/ launch vehicle and Launch Complex 37B functional systems description - environmental conditioning, index of finding numbers, and mechanical schematics
Evaluation of effects of vibrational multiple frequency forcing functions is discussed. Computer program for developing vibrational transfer functions is described. Possible applications of computer program are enumerated.
Saturn I /SA-8/ launch vehicle and Launch Complex 37B - pneumatic distribution system
Saturn I /SA-8/ launch vehicle - environmental control systems, functional description, index of finding numbers, and schematics of launch complex
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - liquid hydrogen fuel system
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - H- 1 rocket engine and hydraulic systems
Saturn I /SA-8/ launch vehicle and launch complex systems - H- 1 rocket engine, and hydraulic systems
Saturn I /SA-8/ launch vehicle and Launch Complex 37B - RL-10 A-3 engine and hydraulic system
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - RL-10 A-3 engine and hydraulic systems
Saturn I /SA-8/ launch vehicle and Launch Complex 37B liquid hydrogen fuel system