Wind Tunnel Investigation Of A Number Of Total Pressure Tubes At High Angles Of Attack
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Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack
| Author | : A. Gerald Rainey |
| Publisher | : |
| Total Pages | : 316 |
| Release | : 1957 |
| Genre | : Aerodynamics |
| ISBN | : |
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The effect of Mach number on both unshielded and shielded tubes was found to be considerable. For most of the unshielded tubes the usable range increased with M
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The National Advisory Committee for Aeronautics is investigating the possibility of designing a fixed total-pressure tube which will remain insensitive to incli
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Calibrations of 39 total-pressure tubes for an angle-of-attack range of plus or minus 45 degrees and an indicated airspeed of the various tubes differed as rega
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Pages: 25
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Calibartions of six shielded total-pressure tubes over an angle-of-attack range of -30 to 65 degrees at Mach numbers of 02.6, 0.50, 0,.70, 0.90, and 0.95 are pr
