Airfoil (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Airfoil" in English language version.

refsWebsite

Global rank English rank

6books.google.com

3^rd place

5harvard.edu

18^th place

17^th place

4doi.org

2^nd place

3semanticscholar.org

11^th place

8^th place

3nasa.gov

75^th place

83^rd place

2web.archive.org

1^st place

2worldcat.org

5^th place

2aerodynamics4students.com

low place

1uni-frankfurt.de

4,572^nd place

7,417^th place

1iop.org

1,725^th place

1,828^th place

1aerospaceweb.org

8,491^st place

8,160^th place

aerodynamics4students.com

Auld & Srinivas 1995: "A simple solution for general two-dimensional aerofoil sections can be obtained by neglecting thickness effects and using a mean-line only section model.... This also means small changes in position are equivalent so that $ds \approx dx$ ." Auld, Douglass; Srinivas (1995). "2-D Thin Aerofoil Theory". Aerodynamics for Students. University of Sydney.
Auld & Srinivas 1995. Auld, Douglass; Srinivas (1995). "2-D Thin Aerofoil Theory". Aerodynamics for Students. University of Sydney.

aerospaceweb.org

Scott 2003: "The equation can only be used for aircraft with medium to large aspect ratio wings and only up to the stall angle, which is usually between 10° and 15° for typical aircraft configurations." Scott, Jeff (10 August 2003). "Question #136: Lift Coefficient & Thin Airfoil Theory". Ask a Rocket Scientist: Aerodynamics. Aerospaceweb.org.

books.google.com

Halliday & Resnick 1988, p. 378: "The effect of the wing is to give the air stream a downward velocity component. The reaction force of the deflected air mass must then act on the wing to give it an equal and opposite upward component." Halliday, David; Resnick, Robert (1988). Fundamentals of Physics (3rd ed.). John Wiley & Sons.
Houghton et al. 2012, p. 18. Houghton, E. L.; Carpenter, P. W.; Collicott, Steven H.; Valentine, Daniel (2012). Aerodynamics for Engineering Students (6th ed.). Elsevier. ISBN 978-0-08-096633-5.
Houghton et al. 2012, p. 17. Houghton, E. L.; Carpenter, P. W.; Collicott, Steven H.; Valentine, Daniel (2012). Aerodynamics for Engineering Students (6th ed.). Elsevier. ISBN 978-0-08-096633-5.
Phillips 2004, p. 27. Phillips, Warren F. (2004). Mechanics of Flight. John Wiley & Sons. ISBN 978-0-471-33458-3.
Abbott & Von Doenhoff 1959, §4.2. Abbott, Ira Herbert; Von Doenhoff, Albert Edward (1959). Theory of Wing Sections, Including a Summary of Airfoil Data. Dover. ISBN 978-0-486-60586-9.
Abbott & Von Doenhoff 1959, §4.3. Abbott, Ira Herbert; Von Doenhoff, Albert Edward (1959). Theory of Wing Sections, Including a Summary of Airfoil Data. Dover. ISBN 978-0-486-60586-9.

doi.org

Babinsky 2003, pp. 497–503: "If a streamline is curved, there must be a pressure gradient across the streamline." Babinsky, Holger (November 2003). "How do wings work?" (PDF). Physics Education. 38 (6): 497–503. Bibcode:2003PhyEd..38..497B. doi:10.1088/0031-9120/38/6/001. S2CID 1657792.
Morris & Rusak 2013, pp. 439–472. Morris, Wallace J.; Rusak, Zvi (October 2013). "Stall onset on aerofoils at low to moderately high Reynolds number flows". Journal of Fluid Mechanics. 733: 439–472. Bibcode:2013JFM...733..439M. doi:10.1017/jfm.2013.440. ISSN 0022-1120. S2CID 122817884.
Traub 2016, p. 9. Traub, Lance W. (24 March 2016). "Semi-Empirical Prediction of Airfoil Hysteresis". Aerospace. 3 (2): 9. Bibcode:2016Aeros...3....9T. doi:10.3390/aerospace3020009.
Ramesh, Kiran; Gopalarathnam, Ashok; Granlund, Kenneth; Ol, Michael V.; Edwards, Jack R. (July 2014). "Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding". Journal of Fluid Mechanics. 751: 500–538. Bibcode:2014JFM...751..500R. doi:10.1017/jfm.2014.297. ISSN 0022-1120. S2CID 121962230.

harvard.edu

ui.adsabs.harvard.edu

Babinsky 2003, pp. 497–503: "If a streamline is curved, there must be a pressure gradient across the streamline." Babinsky, Holger (November 2003). "How do wings work?" (PDF). Physics Education. 38 (6): 497–503. Bibcode:2003PhyEd..38..497B. doi:10.1088/0031-9120/38/6/001. S2CID 1657792.
Morris 2009. Morris, Wallace J. II (2009). A universal prediction of stall onset for airfoils at a wide range of Reynolds number flows (PhD). Harvard University. Bibcode:2009PhDT.......146M.
Morris & Rusak 2013, pp. 439–472. Morris, Wallace J.; Rusak, Zvi (October 2013). "Stall onset on aerofoils at low to moderately high Reynolds number flows". Journal of Fluid Mechanics. 733: 439–472. Bibcode:2013JFM...733..439M. doi:10.1017/jfm.2013.440. ISSN 0022-1120. S2CID 122817884.
Traub 2016, p. 9. Traub, Lance W. (24 March 2016). "Semi-Empirical Prediction of Airfoil Hysteresis". Aerospace. 3 (2): 9. Bibcode:2016Aeros...3....9T. doi:10.3390/aerospace3020009.
Ramesh, Kiran; Gopalarathnam, Ashok; Granlund, Kenneth; Ol, Michael V.; Edwards, Jack R. (July 2014). "Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding". Journal of Fluid Mechanics. 751: 500–538. Bibcode:2014JFM...751..500R. doi:10.1017/jfm.2014.297. ISSN 0022-1120. S2CID 121962230.

iop.org

iopscience.iop.org

Babinsky 2003, pp. 497–503: "If a streamline is curved, there must be a pressure gradient across the streamline." Babinsky, Holger (November 2003). "How do wings work?" (PDF). Physics Education. 38 (6): 497–503. Bibcode:2003PhyEd..38..497B. doi:10.1088/0031-9120/38/6/001. S2CID 1657792.

nasa.gov

ntrs.nasa.gov

Croom, C. C.; Holmes, B. J. (1985-04-01). Flight evaluation of an insect contamination protection system for laminar flow wings.
Holmes, B. J.; Obara, C. J.; Yip, L. P. (1984-06-01). "Natural laminar flow experiments on modern airplane surfaces". NASA Technical Reports.

grc.nasa.gov

Hall, Nancy R. "Lift from Flow Turning". NASA Glenn Research Center. Archived from the original on 5 July 2011. Retrieved 2011-06-29. If the body is shaped, moved, or inclined in such a way as to produce a net deflection or turning of the flow, the local velocity is changed in magnitude, direction, or both. Changing the velocity creates a net force on the body.

semanticscholar.org

api.semanticscholar.org

Babinsky 2003, pp. 497–503: "If a streamline is curved, there must be a pressure gradient across the streamline." Babinsky, Holger (November 2003). "How do wings work?" (PDF). Physics Education. 38 (6): 497–503. Bibcode:2003PhyEd..38..497B. doi:10.1088/0031-9120/38/6/001. S2CID 1657792.
Morris & Rusak 2013, pp. 439–472. Morris, Wallace J.; Rusak, Zvi (October 2013). "Stall onset on aerofoils at low to moderately high Reynolds number flows". Journal of Fluid Mechanics. 733: 439–472. Bibcode:2013JFM...733..439M. doi:10.1017/jfm.2013.440. ISSN 0022-1120. S2CID 122817884.
Ramesh, Kiran; Gopalarathnam, Ashok; Granlund, Kenneth; Ol, Michael V.; Edwards, Jack R. (July 2014). "Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding". Journal of Fluid Mechanics. 751: 500–538. Bibcode:2014JFM...751..500R. doi:10.1017/jfm.2014.297. ISSN 0022-1120. S2CID 121962230.

uni-frankfurt.de

user.uni-frankfurt.de

Weltner & Ingelman-Sundberg 1999. Weltner, Klaus; Ingelman-Sundberg, Martin (1999). "Physics of flight - revisited". Archived from the original on 29 September 2011. Retrieved 25 April 2021.

web.archive.org

Hall, Nancy R. "Lift from Flow Turning". NASA Glenn Research Center. Archived from the original on 5 July 2011. Retrieved 2011-06-29. If the body is shaped, moved, or inclined in such a way as to produce a net deflection or turning of the flow, the local velocity is changed in magnitude, direction, or both. Changing the velocity creates a net force on the body.
Weltner & Ingelman-Sundberg 1999. Weltner, Klaus; Ingelman-Sundberg, Martin (1999). "Physics of flight - revisited". Archived from the original on 29 September 2011. Retrieved 25 April 2021.

worldcat.org

search.worldcat.org

Morris & Rusak 2013, pp. 439–472. Morris, Wallace J.; Rusak, Zvi (October 2013). "Stall onset on aerofoils at low to moderately high Reynolds number flows". Journal of Fluid Mechanics. 733: 439–472. Bibcode:2013JFM...733..439M. doi:10.1017/jfm.2013.440. ISSN 0022-1120. S2CID 122817884.
Ramesh, Kiran; Gopalarathnam, Ashok; Granlund, Kenneth; Ol, Michael V.; Edwards, Jack R. (July 2014). "Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding". Journal of Fluid Mechanics. 751: 500–538. Bibcode:2014JFM...751..500R. doi:10.1017/jfm.2014.297. ISSN 0022-1120. S2CID 121962230.