Experimental Investigation Of The Effects Of Viscosity On The Drag Of Bodies Of Revolution At A Mach Number Of 1 5
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Experimental Investigation of the Effects of Viscosity on the Drag of Bodies of Revolution at a Mach Number of 1 5
Author | : Dean R. Chapman,Edward W. Perkins |
Publsiher | : Unknown |
Total Pages | : 92 |
Release | : 1947 |
Genre | : Aerodynamics |
ISBN | : UFL:31262081065806 |
Download Experimental Investigation of the Effects of Viscosity on the Drag of Bodies of Revolution at a Mach Number of 1 5 Book in PDF, Epub and Kindle
Summary: Tests were conducted to determine the effects of viscosity on the drag and base pressure characteristics of various bodies of revolution at a Mach number of 1.5. The models were tested both with smooth surfaces and with roughness added to evaluate the effects of Reynolds number for both laminar and turbulent boundary layers. The principal geometric variables investigated were after-body shape and length-diameter ratio. For most models, force tests and base pressure measurements were made over a range of Reynolds numbers, based on model length, from 0.6 million to 5.0 millions. Schlieren photographs were used to analyze the effects of viscosity on flow separation and shock-wave configuration near the base and to verify the condition of the boundary layer as deduced from force tests. The results are discussed and compared with theoretical calculations.
A Study of the Use of Experimental Stability Derivatives in the Calculation of the Lateral Disturbed Motions of a Swept wing Airplane and Comparison with Flight Results
Author | : Carl Kaplan,Dean R. Chapman,Jack Fischel,Jackson R. Stalder,John D. Bird,John V. Becker,Marion O. McKinney,Stanley Corrsin,Walter G. Vincenti,United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 294 |
Release | : 1951 |
Genre | : Aerodynamics, Supersonic |
ISBN | : OSU:32435065611311 |
Download A Study of the Use of Experimental Stability Derivatives in the Calculation of the Lateral Disturbed Motions of a Swept wing Airplane and Comparison with Flight Results Book in PDF, Epub and Kindle
Annual Report National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 135 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105024166121 |
Download Annual Report National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Report National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 1462 |
Release | : 1951 |
Genre | : Aeronautics |
ISBN | : CORNELL:31924089884500 |
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Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta a Swept and an Upswept Wing Oscillating in Yaw
Author | : Dean R. Chapman,John R. Spreiter,Lewis R. Fisher,Perry L. Blackshear,Vernon J. Rossow,United States. National Advisory Committee for Aeronautics,Alberta Y. Alksne,Donald M. Kuehn,Howard K. Larson |
Publsiher | : Unknown |
Total Pages | : 206 |
Release | : 1958 |
Genre | : Aerofoils |
ISBN | : OSU:32435063879068 |
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Investigation of the Laminar Aerodynamic Heat transfer Characteristics of a Hemisphere cylinder in the Langley 11 inch Hypersonic Tunnel at a Mach Number of 6 8
Author | : Davis H. Crawford,William D. McCauley |
Publsiher | : Unknown |
Total Pages | : 680 |
Release | : 1956 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105024832029 |
Download Investigation of the Laminar Aerodynamic Heat transfer Characteristics of a Hemisphere cylinder in the Langley 11 inch Hypersonic Tunnel at a Mach Number of 6 8 Book in PDF, Epub and Kindle
At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.