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Calculation of the lateral-dynamic stability of aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| Description | Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for computing the lateral dynamic stability can be determined. A number of numerical examples are given for obtaining the stability derivatives and solving the characteristic-stability equation. Approximate formulas are derived with the aid of which rapid preliminary computations may be made and the stability coefficients corrected for certain modifications of the airplane. A derivation of the lateral-dynamic-stability equations is included. |
| File Size | 2893521 |
| Page Count | 83 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093966 |
| Archival Resource Key | ark:/13960/t19k8pf96 |
| Language | English |
| Publisher Date | 1952-02-01 |
| Access Restriction | Open |
| Subject Keyword | Stability, Lateral - Dynamic Stability - Effect OF Sweepback Stability - Northrop 2e Equations - Motion Equations - Stability Stability, Directional, Dynamic Interference - Wings & Fuselages Stability, Lateral AND Directional - Dynamics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
