Evaluation Of Wind Tunnel Tests On Afmdc Monorail Cone And Spike Nose Sled Configurations At Mach Numbers From 20 To 50
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Author | : W. T Strike (Jr) |
Publisher | : |
Total Pages | : 68 |
Release | : 1968 |
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Download Evaluation of Wind Tunnel Tests on Afmdc Monorail Cone - and Spike-nose Sled Configurations at Mach Numbers from 2.0 to 5.0 Book in PDF, Epub and Kindle
An evaluation was made of the results of wind tunnel tests on 0.4- scale models of two monorail rocket-sled configurations. The sled models consisted of a cylindrical body with forward and aft splitter wedges and slippers and with an interchangeable 15-deg cone nose and spike nose. The wind tunnel tests were conducted at Mach numbers 2, 3, 4, and 5 and over a Reynolds number range (based on the sled body diameter) from 0.22 to 1.92 million. The sled model was sting supported over a scaled replica of the Holloman track rail which was supported on a sharp-leading-edge ground plane (flat plate). The test results consist of static force measurements obtained from a six-component strain-gage balance. Also, pitot pressure flow field surveys were made over the ground plane and model rail in the region occupied by the sled model. The following model parameters were varied during the test: the location of the sled relative to the rail tip and also to the ground plane leading edge, the height of the sled body above the rail surface, the gap between the slipper and rail surface, and the sled roll angle. The results presented include an evaluation of the influence of the sled slippers, the free-stream Reynolds number, and the Mach number on the aerodynamic loading of the sled.
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Total Pages | : 0 |
Release | : 1968 |
Genre | : |
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Download Evaluation of Wind Tunnel Tests on Afmdc Monorail Cone - and Spike-nose Sled Configurations at Mach Numbers from 2.0 to 5.0 Book in PDF, Epub and Kindle
An evaluation was made of the results of wind tunnel tests on 0.4- scale models of two monorail rocket-sled configurations. The sled models consisted of a cylindrical body with forward and aft splitter wedges and slippers and with an interchangeable 15-deg cone nose and spike nose. The wind tunnel tests were conducted at Mach numbers 2, 3, 4, and 5 and over a Reynolds number range (based on the sled body diameter) from 0.22 to 1.92 million. The sled model was sting supported over a scaled replica of the Holloman track rail which was supported on a sharp-leading-edge ground plane (flat plate). The test results consist of static force measurements obtained from a six-component strain-gage balance. Also, pitot pressure flow field surveys were made over the ground plane and model rail in the region occupied by the sled model. The following model parameters were varied during the test: the location of the sled relative to the rail tip and also to the ground plane leading edge, the height of the sled body above the rail surface, the gap between the slipper and rail surface, and the sled roll angle. The results presented include an evaluation of the influence of the sled slippers, the free-stream Reynolds number, and the Mach number on the aerodynamic loading of the sled.
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Total Pages | : 1572 |
Release | : 1969 |
Genre | : Aeronautics |
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Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
Author | : P. J. Bontrager |
Publisher | : |
Total Pages | : 0 |
Release | : 1967 |
Genre | : Aerodynamics, Hypersonic |
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Download Wind Tunnel Tests of Several Third-stage USNOTS Sled Configurations at Mach Numbers 6 and 8 Book in PDF, Epub and Kindle
Author | : William B. Boatright |
Publisher | : |
Total Pages | : 44 |
Release | : 1962 |
Genre | : Wind tunnels |
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Download Description and Preliminary Calibration Tests of a Small Arc-heated Hypersonic Wind Tunnel Book in PDF, Epub and Kindle
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Total Pages | : 34 |
Release | : 1961 |
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Download Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact Book in PDF, Epub and Kindle
Author | : John E. Grimaud |
Publisher | : |
Total Pages | : 44 |
Release | : 1961 |
Genre | : Aerodynamic measurements |
ISBN | : |
Download Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90° Book in PDF, Epub and Kindle
Author | : Maurice A. Sylvester |
Publisher | : |
Total Pages | : 44 |
Release | : 1963 |
Genre | : Launch vehicles (Astronautics) |
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Download Wind Tunnel Tests of the Redstone "B" Nose Cone at Mach Numbers from 1.75 to 5.00 Book in PDF, Epub and Kindle
Author | : Albin O. Pearson |
Publisher | : |
Total Pages | : 40 |
Release | : 1961 |
Genre | : Noses (Space vehicles) |
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Download Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.14 of the Static Aerodynamic Characteristics of Modified Mercury Escape and Exit Capsule Configurations Book in PDF, Epub and Kindle
Author | : Douglas E. Harrington |
Publisher | : |
Total Pages | : 40 |
Release | : 1986 |
Genre | : Mach number |
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Download Experimental Evaluation of Wall Mach Number Distributions of the Octagonal Test Section Proposed for NASA Lewis Research Center's Altitude Wind Tunnel Book in PDF, Epub and Kindle