Call Number (LC) | Title | Results |
---|---|---|
NAS 1.26:182055 | Communication overhead on the Intel iPSC-860 hypercube | 2 |
NAS 1.26:182056 | The preprocessed doacross loop | 2 |
NAS 1.26:182058 |
Software requirements guidance and control software development specification / Software requirements: Guidance and control software development specification |
2 |
NAS 1.26:182061 | On central-difference and upwind schemes | 2 |
NAS 1.26:182062 | A control problem for Burger's equation with bounded input/output | 1 |
NAS 1.26:182063 | Flight service evaluation of composite helicopter components final report February 1981 through November 1990 / | 1 |
NAS 1.26:182064 | Concepts and analysis for precision segmented reflector and feed support structures | 1 |
NAS 1.26:182065 | Structures for remotely deployable precision antennas | 2 |
NAS 1.26:182068 | A critical evaluation of two-equation models for near wall turbulence | 2 |
NAS 1.26:182069 | A real time dynamic data acquisition and processing system for velocity, density, and total temperature fluctuation measurements | 2 |
NAS 1.26:182070 | "Diverter" decision aiding for on-flight diversions | 1 |
NAS 1.26:182071 | On the use of Lagrangian variables in descriptions of unsteady boundary-layer separation | 1 |
NAS 1.26:182072 |
The use of Lanczos's method to solve the large generalized symmetric definite eigenvalue problem in parallel The use of Lanczo's method to solve the large generalized symmetric Eigenvalue problem in parallel |
2 |
NAS 1.26:182073 | Efficient algorithms for a class of partitioning problems | 1 |
NAS 1.26:182074 | Linear iterative solvers for implicit ode methods | 1 |
NAS 1.26:182075 | Laboratory test and acoustic analysis of cabin treatment for propfan test assessment aircraft | 1 |
NAS 1.26:182076 | Aerodynamic preliminary analysis system II | 1 |
NAS 1.26:182077 | Aerodynamic preliminary analysis system II | 1 |
NAS 1.26:182080 | Shock-layer bounds for a singularly perturbed equation | 1 |
NAS 1.26:182081 | Parallelization of implicit finite difference schemes in computational fluid dynamics | 1 |