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An experimental investigation of gapwise periodicity and unsteady aerodynamic response in an oscillating cascade. volume 2: data report. part 2: mode 2 data
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carta, F. O. |
| Copyright Year | 1981 |
| Description | Computer data are provided for tests conducted on a linear cascade of airfoils oscillating in pitch to measure the unsteady pressure response on selected blades along the leading edge plane of the cascade, over the chord of the center blade, and on the sidewall in the plane of the leading edge. |
| File Size | 25243813 |
| Page Count | 388 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820010307 |
| Archival Resource Key | ark:/13960/t1zd2rb83 |
| Language | English |
| Publisher Date | 1981-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Damping Documentation Fourier Analysis Airfoils Aerodynamic Forces Data Reduction Oscillating Flow Printouts Tables Data Cascade Flow Numerical Analysis Unsteady Aerodynamics Wind Tunnel Tests Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |