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

Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack
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Total Pages : 316
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ISBN-10 : OSU:32435063879167
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Book Synopsis Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack by : A. Gerald Rainey

Download or read book Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack written by A. Gerald Rainey and published by . This book was released on 1957 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack
Language: en
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Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack

Authors: A. Gerald Rainey
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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

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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
Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack Subsonic Speeds
Language: en
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Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack Subsonic Speeds

Authors:
Categories:
Type: BOOK - Published: 1951 - Publisher:

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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
Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack
Language: en
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Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack

Authors: William Gracey
Categories: Angle of attack (Aerodynamics)
Type: BOOK - Published: 1951 - Publisher:

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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
Wind-tunnel Investigation of Six Shielded Total-pressure Tubes at High Angles of Attack
Language: en
Pages: 25

Wind-tunnel Investigation of Six Shielded Total-pressure Tubes at High Angles of Attack

Authors: Walter R. Russell
Categories: Aeronautical instruments
Type: BOOK - Published: 1951 - Publisher:

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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