Forsythe, 1949 - Google Patents
Exact particle trajectories for nonviscous flow in a plane with a constant Coriolis parameterForsythe, 1949
View PDF- Document ID
- 9373978869252386845
- Author
- Forsythe G
- Publication year
- Publication venue
- Journal of Atmospheric Sciences
External Links
Snippet
The pressure and density fields are assumed known exactly for all time, and the wind is to be forecast by obtaining the trajectory of each air particle from the equations of nonviscous motion in a plane. The importance of initial conditions is stressed. For sufficiently simple …
- 239000002245 particle 0 title abstract description 13
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06G—ANALOGUE COMPUTERS
- G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
- G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
- G06G7/70—Analogue computers for specific processes, systems or devices, e.g. simulators for vehicles, e.g. to determine permissible loading of ships, centre of gravity, necessary fuel
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06G—ANALOGUE COMPUTERS
- G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
- G06G7/12—Arrangements for performing computing operations, e.g. operational amplifiers
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Batchelor | The conditions for dynamical similarity of motions of a frictionless perfect‐gas atmosphere | |
Louat | On the theory of normal grain growth | |
Rubinow et al. | The transverse force on a spinning sphere moving in a viscous fluid | |
US2968789A (en) | Form recognition system | |
Bažant et al. | Singularities of elastic stresses and of harmonic functions at conical notches or inclusions | |
Klein | Optimal input design for aircraft parameter estimation using dynamicprogramming principles | |
Forsythe | Exact particle trajectories for nonviscous flow in a plane with a constant Coriolis parameter | |
US3147424A (en) | Apparatus for controlling the vertical rate of an aircraft | |
US3791208A (en) | Angle of attack computer | |
Balakrishnan | Modelling and identification theory- A flight control application | |
US2950619A (en) | Flutter simulator | |
Jones | The formation of resonance lines in multidimensional media. I. Scaling properties in two dimensions | |
GB1057562A (en) | Improvements in or relating to air data computers | |
Phong | Global dynamics of the system of two exponential difference equations | |
Berkofsky | Lectures on numerical weather prediction | |
Jezewski | A comparative study of Newtonian, Kustaanheimo/Stiefel, and Sperling/Burdet optimal trajectories | |
Goldsworthy | Supersonic flow over thin symmetrical wings with given surface pressure distribution | |
Bottema | Note on a non-holonomic system | |
Kirszenblat et al. | Least squares nonlinear parameter estimation by the iterative continuation method | |
Marchand | The identification of linear multivariable systems from frequency response data | |
Schwartz | Comment on" An Empirical Expression for Drag Coefficients Cones at Supersonic Speeds" | |
Morrison Jr et al. | Unsteady creeping motion of a sphere at small values of Knudsen number | |
ONGARATO | Subsonic wind tunnel wall interference studies conducted in the NAR trisonic wind tunnel | |
Lefschetz | On automatic controls | |
De Jong | Application of the theory of adjustment to double theodolite observations |