Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Download Further Wind Tunnel Measurements Of Pressure Signatures For A 00041 Scale Model Of The Space Shuttle Orbiter full books in PDF, epub, and Kindle. Read online Further Wind Tunnel Measurements Of Pressure Signatures For A 00041 Scale Model Of The Space Shuttle Orbiter ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author :
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (317 download)
Download or read book Further Wind Tunnel Measurements of Pressure Signatures for a 0.0041-scale Model of the Space Shuttle Orbiter written by and published by . This book was released on 1976 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.:/5 (317 download)
Download or read book Wind Tunnel Pressure Signatures for a 0.0041-scale Model of the Space Shuttle Orbiter written by and published by . This book was released on 1975 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (317 download)
Download or read book Wind Tunnel Pressure Signatures for a .016 Scale Model of the Apollo Command Module written by and published by . This book was released on 1971 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 558 pages
Book Rating : 4.F/5 ( download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1984 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 490 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distributions Obtained on a 0.10-scale Model of the Space Shuttle Orbiter's Forebody in the Ames Unitary Plan Wind Tunnel written by and published by . This book was released on 1986 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (317 download)
Download or read book Near-field Sonic-boom Pressure Signatures for the Space Shuttle Launch and Orbiter Vehicles at Mach 6 written by and published by . This book was released on 1979 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static-pressure signatures parallel to the flight path of the launch and entry configurations of the space shuttle were measured. The launch configurations, consisting of an equivalent body of revolution (representing the orbiter and external fuel tank) with a solid exhaust gas plume attached, was tested at an angle of attack of 0 deg. The entry configuration (orbiter only) was tested over an angle-of-attack range from 10 deg to 40 deg. Calculated pressure signatures were in good agreement with measured signatures for both configurations.
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722698805
Total Pages : 78 pages
Book Rating : 4.6/5 (988 download)
Download or read book Pressure Distributions on a 0. 02-Scale Space Shuttle Orbiter Nose at Mach 21. 5 in Helium written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions on a 0.02-scale model of the Space Shuttle orbiter forward fuselage were obtained in the 22-inch aerodynamic leg of the Langley Hypersonic Helium Tunnel Facility at a nominal free-stream Mach number of 21.5 and a ratio of specific heats of 1.67 for inclusion in the database of the Shuttle entry air data system (SEADS). The data were measured at model angles of attack of 0 deg to 50 deg in 5 deg increments for zero sideslip angle and at model sideslip angles of -5 deg to 5 deg for angles of attack equal to 5, 20, 35, and 40 deg. These data displayed trends similar to those observed in other wind tunnels at Mach 6 and 10 in air. Specifically noted is a shift in the location of the stagnation point at angles of attack above 15 deg; this effect did not, however, occur in flight. By comparison, the data obtained at Mach 6 in the Langley Hypersonic CF4 Tunnel, corresponding to a lower ratio of specific heats in the postshock region than those in helium and air, showed some reduction of the stagnation point shift at the higher angles of attack. The differences between flight and wind tunnel pressure distributions are believed due primarily to high-temperature gas chemistry effects in flight, which include lower effective specific heat ratios but which were not completely duplicated in the wind tunnels. Ashby, George C., Jr. and Bernot, Peter T. and Woods, William C. Langley Research Center...
Author : A. M. Whitnah
Publisher :
ISBN 13 :
Total Pages : 524 pages
Book Rating : 4.F/5 ( download)
Download or read book Space shuttle wind tunnel testing program summary written by A. M. Whitnah and published by . This book was released on 1984 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley 20-inch Mach 6 Air Tunnel written by and published by . This book was released on 1983 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 196 pages
Book Rating : 4.:/5 (317 download)
Download or read book Documentation and Archiving of the Space Shuttle Wind Tunnel Test Data Base. Volume 1: Background and Description written by and published by . This book was released on 1995 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781794283404
Total Pages : 30 pages
Book Rating : 4.2/5 (834 download)
Download or read book Method for Standardizing Sonic-Boom Model Pressure Signatures Measured at Several Wind-Tunnel Facilities written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019-01-19 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Low-boom model pressure signatures are often measured at two or more wind-tunnel facilities. Preliminary measurements are made at small separation distances in a wind tunnel close at hand, and a second set of pressure signatures is measured at larger separation distances in a wind-tunnel facility with a larger test section. In this report, a method for correcting and standardizing the wind-tunnel-measured pressure signatures obtained in different wind tunnel facilities is presented and discussed. Mack, Robert J. Langley Research Center NASA/TM-2007-214854, L-19320
Author : National Aeronautics and Space Administration
Publisher :
ISBN 13 : 9781726202688
Total Pages : 30 pages
Book Rating : 4.2/5 (26 download)
Download or read book An Evaluation of Measured Pressure Signatures from Wind-tunnel Models of Three Low-boom Concepts written by National Aeronautics and Space Administration and published by . This book was released on 2018-08-27 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Revised 1990-1991 sonic-boom design and analysis methodology was assessed by applying it to the design of three low-boom concepts. Models of these concepts were built and used to measure pressure signatures in the wind tunnel. An analysis of wind-tunnel data showed unexpected nacelle-inlet and the nacelle-wing interference-lift shocks in the pressure signatures from the two engine-under-the-wing models, but not in the measured pressure signatures from the wind-tunnel model with the engine nacelles mounted on the aft fuselage. However, additional lift-induced shocks were found in the pressure signature data from all three wind-tunnel models indicating that other flow-field disturbance effects were present.Mack, Robert J.Langley Research CenterSONIC BOOMS; FLOW DISTRIBUTION; DESIGN ANALYSIS; NACELLES; INTERFERENCE LIFT; WIND TUNNEL TESTS; SIGNATURES; WINGS...
Author :
Publisher :
ISBN 13 :
Total Pages : 462 pages
Book Rating : 4.:/5 (317 download)
Download or read book Space Shuttle Phase B Wind Tunnel Model and Test Information. Volume 2: Orbiter Configuration written by and published by . This book was released on 1988 with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William C. Moseley (Jr.)
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)
Download or read book Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)
Download or read book Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley Continuous Flow Hypersonic Tunnel written by and published by . This book was released on 1983 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William F. Denig
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (319 download)
Download or read book Gas Pressure Measurements on Space Shuttle Mission-39 written by William F. Denig and published by . This book was released on 1996 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781720384915
Total Pages : 42 pages
Book Rating : 4.3/5 (849 download)
Download or read book Anomalous Shocks on the Measured Near-Field Pressure Signatures of Low-Boom Wind-Tunnel Models written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-29 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unexpected shocks on wind-tunnel-measured pressure signatures prompted questions about design methods, pressure signature measurement techniques, and the quality of measurements in the flow fields near lifting models. Some of these unexpected shocks were the result of component integration methods. Others were attributed to the three-dimension nature of the flow around a lifting model, to inaccuracies in the prediction of the area-ruled lift, or to wing-tip stall effects. This report discusses the low-boom model wind-tunnel data where these unexpected shocks were initially observed, the physics of the lifting wing/body model's flow field, the wind-tunnel data used to evaluate the applicability of methods for calculating equivalent areas due to lift, the performance of lift prediction codes, and tip stall effects so that the cause of these shocks could be determined.Mack, Robert J.Langley Research CenterPRESSURE MEASUREMENT; WIND TUNNEL TESTS; FLOW DISTRIBUTION; MEASURE AND INTEGRATION; WIND TUNNEL MODELS; BODY-WING CONFIGURATIONS; SIGNATURES; PREDICTIONS; NEAR FIELDS
