Download or read book Calibration of the NASA Glenn Research Center 10 by 10 ft Supersonic Wind Tunnel 1993 and 1995 Tests written by and published by . This book was released on 2000 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Check Calibration of the NASA Glenn 10 by 10 foot Supersonic Wind Tunnel 2014 Test Entry written by Aaron Johnson and published by . This book was released on 2016 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Subsonic Calibration of the NASA Glenn Research Center 10x10 foot Supersonic Wind Tunnel 1998 Tests written by E. Allen Arrington and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Calibration of the NASA Glenn 8 by 6 foot Supersonic Wind Tunnel 1996 and 1997 Tests written by E. Allen Arrington and published by . This book was released on 2012 with total page 113 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low Speed Calibration of the NASA Lewis Research Center 8 by 6 Foot Supersonic Wind Tunnel 1995 Test written by E. Allen Arrington and published by . This book was released on 1997 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Subsonic Flow Quality Surveys of the NASA Lewis Research Center 10 by 10 Foot Supersonic Wind Tunnel written by and published by . This book was released on 1998 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Improved Pressure Measurement System for Calibration of the NASA LeRC 10x10 Supersonic Wind Tunnel written by and published by . This book was released on 1994 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book User Manual for NASA Lewis 10 by 10 Foot Supersonic Wind Tunnel Revised written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: This manual describes the 10- by 10-Foot Supersonic Wind Tunnel at the NASA Lewis Research Center and provides information for users who wish to conduct experiments in this facility. Tunnel performance operating envelopes of altitude, dynamic pressure, Reynolds number, total pressure, and total temperature as a function of test section Mach number are presented. Operating envelopes are shown for both the aerodynamic (closed) cycle and the propulsion (open) cycle. The tunnel test section Mach number range is 2.0 to 3.5. General support systems, such as air systems, hydraulic system, hydrogen system, fuel system, and Schlieren system, are described. Instrumentation and data processing and acquisition systems are also described. Pretest meeting formats and schedules are outlined. Tunnel user responsibility and personnel safety are also discussed. Soeder, Ronald H. Glenn Research Center...

Download or read book Description and Preliminary Calibration Tests of a Small Arc heated Hypersonic Wind Tunnel written by William B. Boatright and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flow Field Surveys of the NASA Lewis Research Center 8 by 6 Foot Supersonic Wind Tunnel 1993 Test written by and published by . This book was released on 1998 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Glenn 1 By 1 Foot Supersonic Wind Tunnel User Manual written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-20 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: This manual describes the NASA Glenn Research Center's 1 - by 1 -Foot Supersonic Wind Tunnel and provides information for customers who wish to conduct experiments in this facility. Tunnel performance envelopes of total pressure, total temperature, and dynamic pressure as a function of test section Mach number are presented. For each Mach number, maps are presented of Reynolds number per foot as a function of the total air temperature at the test section inlet for constant total air pressure at the inlet. General support systems-such as the service air, combustion air, altitude exhaust system, auxiliary bleed system, model hydraulic system, schlieren system, model pressure-sensitive paint, and laser sheet system are discussed. In addition, instrumentation and data processing, acquisition systems are described, pretest meeting formats and schedules are outlined, and customer responsibilities and personnel safety are addressed.Seablom, Kirk D. and Soeder, Ronald H. and Stark, David E. and Leone, John F. X. and Henry, Michael W.Glenn Research CenterMACH NUMBER; REYNOLDS NUMBER; SUPERSONIC WIND TUNNELS; SUPERSONIC FLOW; TEST CHAMBERS; DATA ACQUISITION; MANUALS; WIND TUNNEL NOZZLES; DYNAMIC PRESSURE; WIND TUNNEL TESTS

Download or read book NASA Glenn 1 by 1 Foot Supersonic Wind Tunnel User Manual written by and published by . This book was released on 1999 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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...

Download or read book BASELINE CALIBRATION OF THE NASA LEWIS RESEARCH CENTER 8 BY 6 FOOT SUPERSONIC WIND TUNNEL 1991 AND 1992 TESTS NASA TM 97 107431 AUG 6 1998 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1999* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

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: