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On the temperature distribution behind cylinders in a flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ackeret, Jako |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1959 |
| Abstract | A SIMPLE THEORETICAL EXPLANATION OF THE AERODYNAMIC COOLING OFTEN FOUND NEAR THE BASE AND IN THE WAKE OF BLUFF BODIES IS PRESENTED. THE THEORY IS BASED ON COMPRESSIBLE POTENTIAL FLOW AND MAKES USE OF THE ENERGY INCREMENT ASSOCIATED WITH THE UNSTEADY VELOCITY-POTENTIAL TERM OF THE ENERGY EQUATION IN CALCULATING THE TEMPERATURE AT A POINT IN UNSTEADY FLOW FOR THE GENERAL CASE. THE CASE OF TWO-DIMENSIONAL FLOW PAST A CYLINDER IS EXAMINED IN DETAIL. |
| File Size | 534001 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19980231053 |
| Archival Resource Key | ark:/13960/t03x94r6v |
| Language | English |
| Publisher Date | 1959-08-01 |
| Publisher Institution | NASA (non Center Specific) |
| Access Restriction | Open |
| Subject Keyword | Flight Paths Differential Equations Optimization Aerodynamic Characteristics Vertical Takeoff Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
