Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Wind Tunnel Calibration Of A 40 Conical Pressure Probe At Mach Numbers From 35 To 74
Download Wind Tunnel Calibration Of A 40 Conical Pressure Probe At Mach Numbers From 35 To 74 full books in PDF, epub, and Kindle. Read online Wind Tunnel Calibration Of A 40 Conical Pressure Probe At Mach Numbers From 35 To 74 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Wind-tunnel Calibration of a 40 Degrees Conical Pressure Probe at Mach Numbers from 3.5 to 7.4 by : Frank W. Burcham
Download or read book Wind-tunnel Calibration of a 40 Degrees Conical Pressure Probe at Mach Numbers from 3.5 to 7.4 written by Frank W. Burcham and published by . This book was released on 1968 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Calibration of a 40° Conical Pressure Probe at Mach Numbers from 3.5 to 7.4 by : Frank W. Burcham
Download or read book Wind-tunnel Calibration of a 40° Conical Pressure Probe at Mach Numbers from 3.5 to 7.4 written by Frank W. Burcham and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analysis of Initial Static Pressure Probe Measurements in a Low-density Hypervelocity Wind Tunnel by : David E. Boylan
Download or read book An Analysis of Initial Static Pressure Probe Measurements in a Low-density Hypervelocity Wind Tunnel written by David E. Boylan and published by . This book was released on 1963 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: An initial experimental program was previously conducted to study the problems in using static pressure probes for flow calibration purposes in low- density, hypervelocity wind tunnels with continuous flow. This data is reviewed in the light of more recent data on thermal transpiration. Results indicate that such probes may be used for what might be termed secondary calibrations, but care is required in interpreting the results. The present experiment yielded data which are compared to static pressures calculated from impact- pressure probe calibrations.
Book Synopsis Wind-tunnel Tests of Seven Static-pressure Probes at Transonic Speeds by : Francis J. Capone
Download or read book Wind-tunnel Tests of Seven Static-pressure Probes at Transonic Speeds written by Francis J. Capone and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes mounted very close to the nose of a body of revolution simulating a missile forebody. The tests were conducted at Mach numbers from 0.80 to 1.08 and at angles of attack from -1.7° to 8.4°. The test Reynolds number per foot varied from 3.35 x 106 to 4.05 x 106. For three 4-vane, gimbaled probes, the static-pressure errors remained constant throughout the test angle-of-attack range for all Mach numbers except 1.02. For two single-vane, self-rotating probes having two orifices at ±37.5° from the plane of symmetry on the lower surface of the probe body, the static-pressure error varied as much as 1.5 percent of free-stream static pressure through the test angle-of-attack range for all Mach numbers. For two fixed, cone-cylinder probes of short length and large diameter, the static-pressure error varied over the test angle-of-attack range at constant Mach numbers as much as 8 to 10 percent of free-stream static pressure.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721985128 Total Pages :314 pages Book Rating :4.9/5 (851 download)
Book Synopsis Cone-Probe Rake Design and Calibration for Supersonic Wind Tunnel Models by : National Aeronautics and Space Administration (NASA)
Download or read book Cone-Probe Rake Design and Calibration for Supersonic Wind Tunnel Models written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-27 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of experimental investigations were conducted at the NASA Langley Unitary Plan Wind Tunnel (UPWT) to calibrate cone-probe rakes designed to measure the flow field on 1-2% scale, high-speed wind tunnel models from Mach 2.15 to 2.4. The rakes were developed from a previous design that exhibited unfavorable measurement characteristics caused by a high probe spatial density and flow blockage from the rake body. Calibration parameters included Mach number, total pressure recovery, and flow angularity. Reference conditions were determined from a localized UPWT test section flow survey using a 10deg supersonic wedge probe. Test section Mach number and total pressure were determined using a novel iterative technique that accounted for boundary layer effects on the wedge surface. Cone-probe measurements were correlated to the surveyed flow conditions using analytical functions and recursive algorithms that resolved Mach number, pressure recovery, and flow angle to within +/-0.01, +/-1% and +/-0.1deg , respectively, for angles of attack and sideslip between +/-8deg. Uncertainty estimates indicated the overall cone-probe calibration accuracy was strongly influenced by the propagation of measurement error into the calculated results. Won, Mark J. Ames Research Center 537-07-20...
Book Synopsis Wind-tunnel Calibration Techniques by : Alan Pope
Download or read book Wind-tunnel Calibration Techniques written by Alan Pope and published by . This book was released on 1961 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: Air-flow measuring instruments, their use, and the manner of working up and presenting the data obtained when calibrating low-speed, nearsonic, transonic, supersonic, and hypersonic wind tunnels are discussed. (Author).
Book Synopsis Calibration Report on the University of Michigan Supersonic Wind Tunnel by : P. E. Culbertson
Download or read book Calibration Report on the University of Michigan Supersonic Wind Tunnel written by P. E. Culbertson and published by . This book was released on 1949 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Performance of a Conical Pressure Probe at Mach Numbers of 3.0, 4.5, and 6.0 by : John D. Norris
Download or read book Experimental Performance of a Conical Pressure Probe at Mach Numbers of 3.0, 4.5, and 6.0 written by John D. Norris and published by . This book was released on 1966 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calibration of Transonic and Supersonic Wind Tunnels by : T. D. Reed
Download or read book Calibration of Transonic and Supersonic Wind Tunnels written by T. D. Reed and published by . This book was released on 1977 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN by : H.P. LIEPMAN
Download or read book CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN written by H.P. LIEPMAN and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Baseline Calibration of the NASA Lewis Research Center 8-by 6-Foot Supersonic Wind Tunnel (1991 and 1992 Tests) by :
Download or read book Baseline Calibration of the NASA Lewis Research Center 8-by 6-Foot Supersonic Wind Tunnel (1991 and 1992 Tests) written by and published by . This book was released on 1998 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Calibration Tests and Pressure Measurements on a Blunted Slender Cone from Mach 1.5 to 10.0 by : George K. GARDINER
Download or read book Wind Tunnel Calibration Tests and Pressure Measurements on a Blunted Slender Cone from Mach 1.5 to 10.0 written by George K. GARDINER and published by . This book was released on 1964 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calibration of a 40-inch Continuous Flow Tunnel at Mach Numbers 1.5 to 6 by : C. J. Schueler
Download or read book Calibration of a 40-inch Continuous Flow Tunnel at Mach Numbers 1.5 to 6 written by C. J. Schueler and published by . This book was released on 1959 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Measurements of Surface-pressure Fluctuations at Mach Numbers of 1.6, 2.0, and 2.5 Using 12 Different Transducers by : Thomas L. Lewis
Download or read book Wind-tunnel Measurements of Surface-pressure Fluctuations at Mach Numbers of 1.6, 2.0, and 2.5 Using 12 Different Transducers written by Thomas L. Lewis and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The turbulent boundary layer on the wall of a 9 by 7 foot wind tunnel was measured with 12 different transducers at Mach numbers of 1.6, 2.0, and 2.5. The results indicated that the wall surface-pressure-fluctuation field was more homogeneous at a Mach number of 2.5 than at Mach numbers of 1.6 or 2.0. A comparison of power-spectral-density data at Mach 2.5 with a summary of similar data (Mach 0.1 to 3.45) showed good agreement. The measurement uncertainty was greatest when frequencies were low and the surface-pressure-fluctuation field was homogeneous. The uncertainty at higher frequencies increased as the surface-pressure-fluctuation field became more inhomogeneous. Since transducer mounting effects and system noise levels were determined not to have contributed appreciably to measurement uncertainties, the result was attributed to an interaction between the surface-pressure-fluctuation field and the transducers. Corcos' correction for size effects improved the comparison between transducers at the high frequencies, but did not eliminate an apparent size effect at the lower frequencies.
Book Synopsis Wind-tunnel Pressure Measurements in the Wake of a Cone-cylinder Model at Mach Numbers of 2.30 and 4.65 by : John T. McShera
Download or read book Wind-tunnel Pressure Measurements in the Wake of a Cone-cylinder Model at Mach Numbers of 2.30 and 4.65 written by John T. McShera and published by . This book was released on 1965 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN SUPERSONIC WIND TUNNEL Publisher : ISBN 13 : Total Pages :26 pages Book Rating :4.L/5 ( download)
Book Synopsis P. E. CULBERTSON by : CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN SUPERSONIC WIND TUNNEL
Download or read book P. E. CULBERTSON written by CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN SUPERSONIC WIND TUNNEL and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Scientific and Technical Publications by :
Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
