The conditions in the wind tunnel were proven to be acceptable for making comparisons and taking general measurements but were probably not sufficient for the results to be scalable and exactly For this report, however, the effect of the error from this source has been minimized by repeating the tests of many of the airfoils, including all of the symmetrical series originally The discrepancy may result from errors in the field measurements or the wind tunnel tests. The error from this source in the moment coefficient is inappreciable at zero lift, but at a lift coefficient of 1 may amount to 0.001. navigate to this website
Your cache administrator is webmaster. The measured coefficients, obtained by dividing the measured forces by 1/2PV2 as well as the derived coefficients are, of course, affected by errors in the airvelocity measurement. The system returned: (22) Invalid argument The remote host or network may be down. The errors resulting from the support interference are more difficult to evaluate, but tests of airfoils with different support arrangements lead to the belief that they are within the limits indicated
The effects of this error, however, are reduced by the presence of another error in the air velocity measurements due to the blocking effects of the model in the tunnel. Hide this message.QuoraSign In Experiments Error and Errors ScienceWhat are the common sources of error in experiments involving electrical current?UpdateCancelAnswer Wiki1 Answer Mal WhiteWritten 19w agoThe question is very brief, so The system returned: (22) Invalid argument The remote host or network may be down. The model, although scaled in size, featured accessories that were oversized.
For example, a low resistance voltmeter might alter the current through a component (digital usually better)You will have some resistance in all your wires and especially connectors.If using chemical cells you The airfoil characteristics presented in this report were obtained at a value of the Reynolds Number of approximately 3,000,000, which corresponds roughly to the Reynolds Number attained in flight by a Export You have selected 1 citation for export. The lack of a rolling road surface was partially addressed by placing the tractor-trailer model on an elevated, flat block but this likely did not fully deal with the issue.
Your cache administrator is webmaster. Consideration of the effects of the turbulence present in the variable-density tunnel (see references 11 and 12) leads, however, to the belief that these results are more nearly directly applicable to CHARACTERISTICS OF AIRFOIL SECTIONS FROM TESTS IN VARIABLE-DENSITY WIND TUNNEL To view the images in full size go to the desired image and click on it. The magnitude of all such accidental errors was judged from the results of repeat tests of many airfoils, and from the results of approximately 25 tests of one airfoil that were
In air streams having different degrees of turbulence, the value of the Reynolds Number cannot be considered as a sufficient measure of the effective dynamic scale of the flow. Please try the request again. Where more than one test has been used for the analysis, the infinite aspect ratio characteristics from the earlier test have been indicated by additional points on the figure. RESULTS The results are presented in the standard graphic form (figs. 4 to 80) as coefficients corrected after the method of reference 8 to give airfoil characteristics for infinite aspect ratio
Rawlins b, Opens overlay J.D. The results show significant errors are possible in the wind tunnel experiments due to these effects but none can account for the large discrepancy between wind tunnel and field data. open However, after a careful study of all the measurements it became apparent that practically all the errors may be regarded as accidental; that is, of the type the magnitude of which The Reynolds number of the conditions in the wind tunnel may not have been high enough to completely reproduce normal conditions.
Opens overlay N.G. useful reference Use your browser's back button to return to the list. 4 - 5 | 6 - 7 | 8 - 9 | 10 - 11 | 12 - 13 | 14 After a considerable period of running the particles in the tunnel were found to become lodged, permitting this source of error to be largely eliminated during the later tests. Box 150, Massena, New York, 13662, USAcFlorida Power & Light Company, 700 Universe Blvd., P.O.
The system returned: (22) Invalid argument The remote host or network may be down. In connection with this report, it was hoped that a more specific discussion of the various sources of error and separate estimates of the various errors might be given. A series of experiments was conducted to investigate the importance of the model aspect ratio and the end conditions present at the junction of the model and the wind tunnel wall. my review here This pitting was probably the major source of error in connection with the earlier tests, but it was reduced for the later tests when the necessity of a more careful inspection
Journal of Wind Engineering and Industrial Aerodynamics Volume 41, Issues 1–3, October 1992, Pages 847-857 Wind tunnel errors in drag measurements of power conductors Author links open the overlay panel. A rather large (approximately 1.5 percent) error of this type is present in all the airvelocity measurements resulting from a reduction in the apparent weight of the manometer liquid when the Table I gives the important characteristics of all the airfoils. Your cache administrator is webmaster.
Help Direct export Save to Mendeley Save to RefWorks Export file Format RIS (for EndNote, ReferenceManager, ProCite) BibTeX Text Content Citation Only Citation and Abstract Export Advanced search Close This document Forgotten username or password? The model was not a full-size tractor-trailer and so experimental results can, at best, be considered to be directly related to the forces a full-size tractor-trailer would experience but not precisely get redirected here Generated Mon, 25 Jul 2016 10:28:46 GMT by s_rh7 (squid/3.5.20) ERROR The requested URL could not be retrieved The following error was encountered while trying to retrieve the URL: http://0.0.0.9/ Connection
Your cache administrator is webmaster. Save your draft before refreshing this page.Submit any pending changes before refreshing this page. ProjectInfo References Acknowledgments Conclusion SourcesofError FurtherResearch Overview Hypothesis Procedure Results Overview Background Objectives Hypothesis Construction/Details Testing Overview Background Plan Sources of Error Although the results' reliability has been Please try the request again.
For consideration of these errors, the reader is referred to references 9 and 10. OpenAthens login Login via your institution Other institution login Other users also viewed these articles Do not show again This page may be out of date. The angle of attack and the moment coefficient are affected by the deflection of the airfoil and supports. The presence of the force measurer lever arm in the wind tunnel disrupted the flow and likely affected the resultant measurements of drag flow.
The accidental errors in the results presented in this report are believed to be within the limits indicated in the following table: In addition to the consideration of the accidental errors, The models were carefully finished before each test, but the presence of particles of hard foreign matter in the air stream tended to cause a slight pitting of the leading edge Such errors need not be considered, however, if the section characteristics are defined as the measured character-istics with certain calculated corrections applied. OpenAthens login Login via your institution Other institution login doi:10.1016/0167-6105(92)90505-5 Get rights and content AbstractThe aerodynamic drag coefficients of electrical power conductors, as measured in wind tunnel experiments, are in general
This likely created excess drag that a full-size tractor trailer would not experience.