Gotowe bibliografie tematyczne / Shockwave Boundary Layer Interactions

Spis treści

  1. Artykuły w czasopismach
  2. Rozprawy doktorskie
  3. Książki
  4. Części książek
  5. Streszczenia konferencji
  6. Raporty organizacyjne

Gotowa bibliografia na temat „Shockwave Boundary Layer Interactions”

Autor: Grafiati
Data publikacji: 6 września 2023

Utwórz poprawne odniesienie w stylach APA, MLA, Chicago, Harvard i wielu innych

Wybierz rodzaj źródła:

Zobacz listy aktualnych artykułów, książek, rozpraw, streszczeń i innych źródeł naukowych na temat „Shockwave Boundary Layer Interactions”.

Przycisk „Dodaj do bibliografii” jest dostępny obok każdej pracy w bibliografii. Użyj go – a my automatycznie utworzymy odniesienie bibliograficzne do wybranej pracy w stylu cytowania, którego potrzebujesz: APA, MLA, Harvard, Chicago, Vancouver itp.

Możesz również pobrać pełny tekst publikacji naukowej w formacie „.pdf” i przeczytać adnotację do pracy online, jeśli odpowiednie parametry są dostępne w metadanych.

Artykuły w czasopismach na temat "Shockwave Boundary Layer Interactions"

1

Chokani, N., and L. C. Squire. "Transonic shockwave/turbulent boundary layer interactions on a porous surface." Aeronautical Journal 97, no. 965 (1993): 163–70. http://dx.doi.org/10.1017/s0001924000026117.

Pełny tekst źródła
Streszczenie:
AbstractTransonic shockwave/turbulent boundary layer interactions on a porous surface above a closed plenum chamber have been studied experimentally in the choked flow of a windtunnel test-section. The equivalent freestream Mach number is 0.76 and results were obtained for three shock strengths. Without the porous surface the Mach numbers ahead of the shock were 1.13, 1.18 and 1.26. The respective shock Mach numbers with the porous surface were 1.10, 1.11 and 1.19. Laser holographic interferometry results are used to measure the density flowfield and examine the nature of the interaction. Thes
Style APA, Harvard, Vancouver, ISO itp.
2

Chand, S. V. S. A. Hema Sai. "Transonic shockwave/boundary layer interactions on NACA 5 series -24112." International Journal of Current Engineering and Technology 2, no. 2 (2010): 629–34. http://dx.doi.org/10.14741/ijcet/spl.2.2014.120.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Hanna, Rebecca L. "Hypersonic shockwave/turbulent boundary-layer interactions on a porous surface." AIAA Journal 33, no. 10 (1995): 1977–79. http://dx.doi.org/10.2514/3.12755.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

Sebastian, Jiss J., and Frank K. Lu. "Upstream-Influence Scaling of Fin-Induced Laminar Shockwave/Boundary-Layer Interactions." AIAA Journal 59, no. 5 (2021): 1861–64. http://dx.doi.org/10.2514/1.j059354.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Délery, J. M. "Shock phenomena in high speed aerodynamics: still a source of major concern." Aeronautical Journal 103, no. 1019 (1999): 19–34. http://dx.doi.org/10.1017/s0001924000065076.

Pełny tekst źródła
Streszczenie:
Abstract Shockwaves are present in a flow as soon as the Mach number becomes supersonic. Being viscous phenomena, Shockwaves are a source of drag which can be predominant when the Mach number is significantly higher than one. In supersonic air intakes, the production of entropy by shocks is felt as a loss in efficiency. At high Mach numbers, Shockwaves produce a considerable temperature rise leading to severe heating problems, complicated by real gas effects. The intersection - or interference - of two shocks gives rise to complex wave patterns containing slip-lines and associated shear layers
Style APA, Harvard, Vancouver, ISO itp.
6

Zahrolayali, Nurfathin, Mohd Rashdan Saad, Azam Che Idris, and Mohd Rosdzimin Abdul Rahman. "Assessing the Performance of Hypersonic Inlets by Applying a Heat Source with the Throttling Effect." Aerospace 9, no. 8 (2022): 449. http://dx.doi.org/10.3390/aerospace9080449.

Pełny tekst źródła
Streszczenie:
Utilization of a heat source to regulate the shock wave–boundary layer interaction (SWBLI) of hypersonic inlets during throttling was computationally investigated. A plug was installed at the intake isolator’s exit, which caused throttling. The location of the heat source was established by analysing the interaction of the shockwave from the compression ramp and the contact spot of the shockwave with that of the inlet cowl. Shockwave interaction inside the isolator was investigated using steady and transient cases. The present computational work was validated using previous experimental work.
Style APA, Harvard, Vancouver, ISO itp.
7

Grilli, Muzio, Peter J. Schmid, Stefan Hickel, and Nikolaus A. Adams. "Analysis of unsteady behaviour in shockwave turbulent boundary layer interaction." Journal of Fluid Mechanics 700 (February 28, 2012): 16–28. http://dx.doi.org/10.1017/jfm.2012.37.

Pełny tekst źródła
Streszczenie:
AbstractThe unsteady behaviour in shockwave turbulent boundary layer interaction is investigated by analysing results from a large eddy simulation of a supersonic turbulent boundary layer over a compression–expansion ramp. The interaction leads to a very-low-frequency motion near the foot of the shock, with a characteristic frequency that is three orders of magnitude lower than the typical frequency of the incoming boundary layer. Wall pressure data are first analysed by means of Fourier analysis, highlighting the low-frequency phenomenon in the interaction region. Furthermore, the flow dynami
Style APA, Harvard, Vancouver, ISO itp.
8

Hamed, A., and J. S. Shang. "Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets." Journal of Propulsion and Power 7, no. 4 (1991): 617–25. http://dx.doi.org/10.2514/3.23370.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
9

Sznajder, Janusz, and Tomasz Kwiatkowski. "EFFECTS OF TURBULENCE INDUCED BY MICRO VORTEX GENERATORS ON SHOCKWAVE – BOUNDARY LAYER INTERACTIONS." Journal of KONES. Powertrain and Transport 22, no. 2 (2015): 241–48. http://dx.doi.org/10.5604/12314005.1165445.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

Kalra, Chiranjeev S., Sohail H. Zaidi, Richard B. Miles, and Sergey O. Macheret. "Shockwave–turbulent boundary layer interaction control using magnetically driven surface discharges." Experiments in Fluids 50, no. 3 (2010): 547–59. http://dx.doi.org/10.1007/s00348-010-0898-9.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.

Rozprawy doktorskie na temat "Shockwave Boundary Layer Interactions"

1

Leung, Andrew Wing Che. "An investigation of three-dimensional shockwave/turbulent-boundary layer interaction." Thesis, University of Cambridge, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.284191.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
2

Galbraith, Daniel S. "Computational Fluid Dynamics Investigation into Shock Boundary Layer Interactions in the “Glass Inlet” Wind Tunnel." University of Cincinnati / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1322053278.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Bellinger, James. "Control of the oblique shockwave/boundary layer interaction in a supersonic inlet." Connect to resource, 2008. http://hdl.handle.net/1811/32065.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

Chokani, Ndaona. "A study of the passive effect on transonic shockwave/turbulent boundary layer interactions on porous surfaces." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.293606.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Bunnag, Shane. "Bleed Rate Model Based on Prandtl-Meyer Expansion for a Bleed Hole Normal to a Supersonic Freestream." University of Cincinnati / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1282330691.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
6

Grilli, Muzio [Verfasser], Nikolaus A. [Akademischer Betreuer] Adams, and Roberto [Akademischer Betreuer] Verzicco. "Analysis of the unsteady behavior in shockwave turbulent boundary layer interaction / Muzio Grilli. Gutachter: Roberto Verzicco ; Nikolaus A. Adams. Betreuer: Nikolaus A. Adams." München : Universitätsbibliothek der TU München, 2013. http://d-nb.info/1046404741/34.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
7

Boyer, Nathan Robert. "The Effects of Viscosity and Three-Dimensionality on Shockwave-Induced Panel Flutter." The Ohio State University, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu156616766854713.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
8

Philit, Mickaël. "Modélisation, simulation et analyse des instationnarités en écoulement transsonique décollé en vue d'application à l'aéroélasticité des turbomachines." Thesis, Ecully, Ecole centrale de Lyon, 2013. http://www.theses.fr/2013ECDL0033/document.

Pełny tekst źródła
Streszczenie:
Dans la conception des turbomachines modernes, la prédiction des phénomènes aéroélastiques est devenue un point clé. La tendance à réduire la masse et à augmenter la charge des composants aérodynamiques accroit le risque de rupture. Dans un tel contexte, la compréhension et la bonne prédiction des diverses instabilités constituent un enjeu industriel et scientifique majeur. Le présent travail de recherche a pour objectif d’améliorer la prédiction des phénomènes instationnaires intervenant dans les problèmes d’aéroélasticité en turbomachines. Cette thèse est plus particulièrement axée sur la si
Style APA, Harvard, Vancouver, ISO itp.
9

Frank, Donya P. "Wave-Current Bottom Boundary Layer Interactions." The Ohio State University, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=osu1229087949.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

Touber, Emile. "Unsteadiness in shock-wave/boundary layer interactions." Thesis, University of Southampton, 2010. https://eprints.soton.ac.uk/161073/.

Pełny tekst źródła
Streszczenie:
The need for better understanding of the low-frequency unsteadiness observed in shock wave/turbulent boundary layer interactions has been driving research in this area for several decades. This work investigates the interaction between an impinging oblique shock and a supersonic turbulent boundary layer via large-eddy simulations. Special care is taken at the inlet in order to avoid introducing artificial low-frequency modes that could affect the interaction. All simulations cover extensive integration times to allow for a spectral analysis at the low frequencies of interest. The simulations b
Style APA, Harvard, Vancouver, ISO itp.

Książki na temat "Shockwave Boundary Layer Interactions"

1

R, Hingst W., and United States. National Aeronautics and Space Administration., eds. Surface and flow field measurements in a symmetric crossing shockwave/turbulent boundary-layer interaction. National Aeronautics and Space Administration, 1993.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
2

Délery, J. Shock-wave boundary layer interactions. NATO, Advisory Group for Aerospace Research and Development, 1986.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Babinsky, Holger, and John K. Harvey, eds. Shock Wave–Boundary-Layer Interactions. Cambridge University Press, 2011. http://dx.doi.org/10.1017/cbo9780511842757.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

Shock wave-boundary layer interactions. Cambridge University Press, 2011.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Delery, J. Shock-wave boundary layer interactions. Agard, 1986.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
6

IUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Edited by Délery J. 1939-, International Union of Theoretical and Applied Mechanics., and France. Office national d'études et de recherches aérospatiales. Springer-Verlag, 1986.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
7

Arellano, Jordi Vilà-Guerau de. Atmospheric boundary layer: Integrating air chemistry and land interactions. Cambridge University Press, 2015.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
8

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. National Aeronautics and Space Administration, Langley Research Center, 1993.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
9

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Institute for Computer Applications in Science and Engineering, 1993.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

United States. National Aeronautics and Space Administration., ed. Experimental studies of hypersonic shock-wave boundary-layer interactions. University of Texas at Arlington, 1992.

Znajdź pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.

Części książek na temat "Shockwave Boundary Layer Interactions"

1

Lusher, D. J., and N. D. Sandham. "Shockwave/Boundary-Layer Interactions in Transitional Rectangular Duct Flows." In ERCOFTAC Series. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-42822-8_35.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
2

Bogdonoff, S. M. "Observation of Three-dimensional “Separation” in Shock Wave Turbulent Boundary Layer Interactions." In Boundary-Layer Separation. Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-83000-6_3.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Kaushik, Mrinal. "Shock Wave and Boundary Layer Interactions." In Theoretical and Experimental Aerodynamics. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-1678-4_14.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

Sandholt, Per Even, and Charles J. Farrugia. "The aurora as monitor of solar wind-magnetosphere interactions." In Earth's Low-Latitude Boundary Layer. American Geophysical Union, 2003. http://dx.doi.org/10.1029/133gm34.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Hultqvist, B., R. Lundin, and K. Stasiewicz. "Ion Interactions in the Magnetospheric Boundary Layer." In Geophysical Monograph Series. American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm038p0127.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
6

Bai, H. L., Y. Zhou, and W. G. Zhang. "Streaky Structures in a Controlled Turbulent Boundary Layer." In Fluid-Structure-Sound Interactions and Control. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-40371-2_19.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
7

Szwaba, Ryszard, Piotr Doerffer, and Piotr Kaczynski. "Transition Effect on Shock Wave Boundary Layer Interaction on Compressor Blade." In Shock Wave Interactions. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-73180-3_2.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
8

Brown, J. L., M. I. Kussoy, and T. J. Coakley. "Turbulent Properties of Axisymmetric Shock-Wave/Boundary-Layer Interaction Flows." In Turbulent Shear-Layer/Shock-Wave Interactions. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9_12.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
9

Saida, N. "Separation ahead of Blunt Fins in Supersonic Turbulent Boundary-Layers." In Turbulent Shear-Layer/Shock-Wave Interactions. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9_20.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

Smits, Alexander J., and Seymour M. Bogdonoff. "A “Preview” of Three-Dimensional Shock-Wave/ Turbulent Boundary-Layer Interactions." In Turbulent Shear-Layer/Shock-Wave Interactions. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9_16.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.

Streszczenia konferencji na temat "Shockwave Boundary Layer Interactions"

1

Murray, Neil, and Richard Hillier. "Separated Shockwave / Turbulent Boundary Layer Interactions at Hypersonic Speeds." In 36th AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3038.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
2

Hanna, Rebecca. "Hypersonic shockwave/turbulent boundary layer interactions on a porous surface." In 33rd Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-5.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Sivasubramanian, Jayahar, and Hermann F. Fasel. "Numerical Investigation of Shockwave Boundary Layer Interactions in Supersonic Flows." In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-0613.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

HORSTMAN, C. "Computation of sharp-fin-induced shockwave/turbulent boundary layer interactions." In 4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1032.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Priebe, Stephan, and Pino Martin. "Direct Numerical Simulation of Shockwave and Turbulent Boundary Layer Interactions." In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-589.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
6

Lee, Sunyoung, and Andreas Gross. "Numerical Investigation of Super- and Hypersonic Laminar Shockwave Boundary Layer Interactions." In AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3441.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
7

Sebastian, Jiss J., and Frank K. Lu. "Upstream-Influence Scaling of Fin-Generated Shockwave/Laminar Boundary-Layer Interactions." In AIAA AVIATION 2020 FORUM. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-3009.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
8

Murray, Neil, and Richard Hillier. "Hypersonic ShockWave/Turbulent Boundary Layer Interactions In A Three-Dimensional Flow." In 44th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-121.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
9

Cohen, Daniel, and Konstantinos Kontis. "Passive Control of Shockwave-Boundary Layer Interactions Using Ultrasonically Absorptive Surfaces." In 42nd AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1059.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

Tripathi, Akriti, Lee Mears, Kourosh Shoele, and Rajan Kumar. "Oblique Shockwave Boundary Layer Interactions on a Flexible Panel at Mach 2." In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-0568.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.

Raporty organizacyjne na temat "Shockwave Boundary Layer Interactions"

1

Martin, M. P., and A. J. Smits. Understanding and Predicting Shockwave and Turbulent Boundary Layer Interactions. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada504718.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
2

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada531259.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
3

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions In Boundary Layer Clouds. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada532783.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
4

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada541857.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
5

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada574045.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
6

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada575522.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
7

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada598037.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
8

Albrecht, Bruce. Aerosol-Cloud-Drizzle-Turbulence Interactions in Boundary Layer Clouds. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada557114.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
9

Loth, Eric, and Sang Lee. Understanding Micro-Ramp Control for Shock Boundary Layer Interactions. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada478600.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
10

Dolling, D. S., N. C. Clemens, and E. Hood. Exploratory Experimental Study of Transitional Shock Wave Boundary Layer Interactions. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada411523.

Pełny tekst źródła
Style APA, Harvard, Vancouver, ISO itp.
Oferujemy zniżki na wszystkie plany premium dla autorów, których prace zostały uwzględnione w tematycznych zestawieniach literatury. Skontaktuj się z nami, aby uzyskać unikalny kod promocyjny!

Do bibliografii