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Wind Tunnel Investigation Of A Number Of Total Pressure Tubes At High Angles Of Attack
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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:
Book Synopsis Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack by : William Gracey
Download or read book Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack written by William Gracey and published by . This book was released on 1957 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 Mach number, whereas that of the shielded tubes decreased with Mach number.
Book Synopsis Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack Subsonic Speeds by :
Download or read book Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack Subsonic Speeds written by and published by . This book was released on 1951 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Advisory Committee for Aeronautics is investigating the possibility of designing a fixed total-pressure tube which will remain insensitive to inclination of the air stream over a wide range of angle of attack throughout the subsonic and supersonic speed ranges. As the first step in this program the variation of total-pressure error with angle of attack of 39 total-pressure tubes has been determined for an angle-of-attack range of + or - 45 deg and an indicated airspeed of 195 miles per hour. The design of these tubes was varied in such a manner that the effects of external shape, internal shape, and configuration of the total- pressure entry could be determined. The external shapes tested included cylindrical-, conical-, and ogival-nose sections. The internal shapes and total-pressure entries were varied on the basis of such factors as size of impact opening, shape of internal chamber, internal bevel, leading-edge sharpness, slant profile, and shielding (combined with venting).
Book Synopsis Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack by : William Gracey
Download or read book Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack written by William Gracey and published by . This book was released on 1951 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 regards external shape, internal shape, and type of total-pressure entry. External shapes testsed included cylindrical-, conical-, and ogival-nose sections. Internal shapes and total-pressure entries were varied on the basis of such factors as size of impact opening, leading-edge sharpness, chamber shape, internal bevel, slant profile, and shielding (combined with venting). The effect of these design variables on the sensitivity of the tubes to angle of attack is discussed.
Book Synopsis Wind-tunnel Investigation of Six Shielded Total-pressure Tubes at High Angles of Attack by : Walter R. Russell
Download or read book Wind-tunnel Investigation of Six Shielded Total-pressure Tubes at High Angles of Attack written by Walter R. Russell and published by . This book was released on 1951 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 presented. One of these tubes was a standard Kiel design, while the other tubes were variations of this design. The design variables which were investigated included the shape of the venturi entry (conical and curved), the position of the total-pressure probe with respect to the leading edge of the shield, the internal diameter of the shield, and the shape of the leading-edge profile. The effect of these variables on the range of angle of attack over which the tubes remained insensitve to inclination is discussed.
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Speed Wind Tunnel Testing by : Alan Pope
Download or read book High Speed Wind Tunnel Testing written by Alan Pope and published by John Wiley & Sons. This book was released on 1965-01-15 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Wind-tunnel Investigation of Errors Indicated by Total-pressure Tubes in the Flow Field of a Body Simulating the Nose of the X-15 Research Airplane by : William J. Alford
Download or read book Subsonic Wind-tunnel Investigation of Errors Indicated by Total-pressure Tubes in the Flow Field of a Body Simulating the Nose of the X-15 Research Airplane written by William J. Alford and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 1056 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of N.A.C.A. 23012, 23021, and 23030 Airfoils with Various Sizes of Split Flap by : Carl Joseph Wenzinger
Download or read book Wind-tunnel Investigation of N.A.C.A. 23012, 23021, and 23030 Airfoils with Various Sizes of Split Flap written by Carl Joseph Wenzinger and published by . This book was released on 1940 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note written by and published by . This book was released on 1951 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by and published by . This book was released on 1958 with total page 1138 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy by : Robert F. Smiley
Download or read book Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy written by Robert F. Smiley and published by . This book was released on 1956 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of systematic approximations to the summary theory is developed for the treatment of problems too simple to merit the use of the complete summary theory, and procedures are discussed for applying the summary theory and its systematic approximations to the shimmy of more complex landing-gear structures than have previously been considered.
Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 852 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Download or read book NASA Technical Note written by and published by . This book was released on 1966 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
