[
[1] Sagalovich, A.V., Kononikhin, A.V., Popov, V.V., Dudnik, S.F., Sagalovich, V.V., 2011, “Eksperimental’nyye issledovaniya pokrytiy tipa Avinit” [Experimental studies of Avinit type coatings], Aviacionno-Kosmicheskaya Tekhnika i Tekhnologiya, 3, pp. 5–15. http://nbuv.gov.ua/UJRN/aktit_2011_3_3.
]Search in Google Scholar
[
[2] Sagalovich, O.V., Kononikhin O.V., V.V. Popov, 2010, “Ustanovka Avinit dlya naneseniya mnogoslojnyh funkcional’nyh pokrytij” [Avinit installation for application of multilayer functional coverings], Physical Surface Engineering, 8, pp. 336–347. http://dspace.nbuv.gov.ua/handle/123456789/98914.
]Search in Google Scholar
[
[3] Sagalovich, A.V., Kononikhin, A.V., Popov, V.V., 2011, “Issledovanie tribologicheskih harakteristik mnogoslojnyh pokrytij MO-S, poluchennyh gazofaznym metodom s ispol’zovaniem metalloorganicheskih soedinenij” [Study of the multilayer MO-C coatings tribological characteristics obtained by the gas-phase method using organometallic compounds], HNADU Bulletin, 54, pp. 44–51.
]Search in Google Scholar
[
[4] Fetisov, V.S., Neugodnikova, L.M., Adamovskii, V.V., Krasnoperov R.A., 2014, Bespilotnaya aviaciya: terminologiya, klassifikaciya, sovremennoe sostoyanie [Unmanned aircraft: terminology, classification, current state], Ufa, FOTON.
]Search in Google Scholar
[
[5] Bashinskij, V.G., Bzot, V.B., Zhilin, E.I., Katunin, A.N., Leont’ev, A.B., Ryb’yak, A.S., Ukrainec, E.A., Hrapchinskij, V.O., Hudov G.V., 2014, Malogabaritnye bespilotnye aviacionnye kompleksy (monografiya) [Small-sized unmanned aerial systems (monograph)]. Zaporizhzhia, “JSC Motor Sich”, p. 262. http://www.hups.mil.gov.ua/periodic-app/monograph/2014/85.
]Search in Google Scholar
[
[6] Rankine, W.J., 1865, On the Mechanical Principles of the Action of Propellers, 4th ed., Transactions of the Institute of Naval Architects, pp. 13–39. https://www.worldcat.org/title/on-the-mechanical-principles-of-the-action-of-propellers/oclc/40237703.
]Search in Google Scholar
[
[7] Gubskij, V.V. 2017, Interferenciya vozdushnyh vintov s elementami planera i mekhanizaciej kryla legkogo transportnogo samoleta na rezhimah vzleta i posadki [Interference of propellers with airframe elements and wing mechanization of a light transport aircraft in take-off and landing modes], Ph.D. thesis, TsAGI, Zhukovsky, Chap. 5, pp. 82–96. https://www.dissercat.com/content/interferentsiyavozdushnykh-vintov-s-elementami-planera-i-mekhanizatsiei-kryla-legkogo-trans.
]Search in Google Scholar
[
[8] Wood, D.H, Bioletti, C., 1934, Tests of Nacelle-Propeller Combinations in Various Positions with Reference to Wings. Part VI. Wings and Nacelles with Pusher Propeller. NACA TR-507, pp. 619–649.
]Search in Google Scholar
[
[9] Borin, A.A., 1970, Vliyanie obduvki chastej samoleta struej ot vinta na harakteristiki vzleta i razbega [Influence of propeller jet blowing of aircraft parts on take-off and take-off run characteristics], TsAGI, Zhukovsky, 1278, p. 16.
]Search in Google Scholar
[
[10] Zolotko, E.M., 1984, Pod”emnaya sila kryla, obduvaemogo struej ot vintov, pri izmenenii koefficienta nagruzki na ometaemuyu vintom ploshchad’ ot 0 do ∞ [The lifting force of the wing blown by the jet from the propellers, when the load factor on the propeller-swept area changes from 0 ti ∞], TsAGI, Zhukovsky, 2235, pp. 3–10.
]Search in Google Scholar
[
[11] Naumov, S.Y., Pustovoitov, V.P., Rudenia, V.I., 1971, Metodika rascheta vliyaniya vozdushnyh vintov na aerodinamicheskie harakteristiki samoleta [Method for calculating the propellers effect on the aerodynamic characteristics of an aircraft], TsAGI, Zhukovsky, 1312, p. 40.
]Search in Google Scholar
[
[12] Ukrainets, E.A., 1998, Aerodinamicheskie harakteristiki nesushchih sistem letatel’nyh apparatov s soosnymi vintovymi dvizhitelyami [Aerodynamic characteristics of the aircraft bearing systems with coaxial propellers] Ph.D. thesis, National Aviation University, Kyiv, p. 148. http://lawdiss.org.ua/ard/99ueosgr.shtml.
]Search in Google Scholar
[
[13] Myrhorod, Y.I., Kalkamanov, S.A., Ukrainets, E.A., 1998, “Doslidzhennia vplyvu kilkosti lopatei na stupin nestatsionarnosti strumenia za hvyntovym rushiiem” [Investigation of the influence of the number of blades on the degree of non-stationarity of the jet on the propeller], Zbirnyk. nauk. prats Kharkivskogo instituty liotchkiv, 2, pp. 44–47.
]Search in Google Scholar
[
[14] Gotsak, V.V., Ukrainets, E.A., 2003, “Metodyka rozrakhunku aerodynamichnykh kharakterystyk skladnykh komponuvan” [Method of calculating the aerodynamic characteristics of complex configurations], Zbirnyk. nauk. prats Kharkivskogo instituty liotchkiv, 1(9), pp. 11–16.
]Search in Google Scholar
[
[15] Deryshev, S.G., 2000, Aerodinamicheskaya interferenciya vozdushnyh vintov i planera dvuhdvigatel’nogo samoleta [Aerodynamic interference of propellers and glider of a twin-engine aircraft], Ph.D. thesis, Siberian Research Institute of Aviation, p. 171. https://www.dissercat.com/content/aerodinamicheskaya-interferentsiya-vozdushnykh-vintov-iplanera-dvukhdvigatelnogo-samoleta.
]Search in Google Scholar
[
[16] Lemko, O.L., 2002, “Letayushchie kryl’ya” [Flying wings – History and Possible Ways of Development], NTs VVTs VCU, p. 91. https://ela.kpi.ua/bitstream/123456789/7834/1/pap_14.pdf.
]Search in Google Scholar
[
[17] Lukov, G.I., Kiseleva, A.M., 1987, “Issledovanie pri malyh skorostyah fizicheskoj kartiny raspredeleniya zavihrennosti potoka okolo modelej samoleta skhem ‘beskhvostka’ i ‘utka’ s krylom malogo udlineniya” [Physical pattern investigation at low speeds of the distribution of flow vorticity near the aircraft models of the “tailless” and “duck” schemes with a wing of small elongation], TsAGI, Zhukovsky, 2341, pp. 3–29.
]Search in Google Scholar
[
[18] Degani, D., Mareus, S.W., 1997, “Thin vs full Navier-Stokes computation for high-angle-of-attack aerodynamics” AIAA Journal, 35(3), pp. 565–567. https://link.springer.com/chapter/10.1007/978-1-4612-2824-0_910.2514/2.134
]Search in Google Scholar
[
[19] Koval, M.O., Kalkamanov, S.A., Chygryn, R.M., 2004, “Aerodinamichni komponovki perspektivnih litakiv vertikal’nogo zl’otu ta posadki” [Aerodynamic layouts of promising vertical takeoff and landing aircraft], Issues of design and manufacture of aircraft structures, National Aerospace University “Kharkiv Aviation Institute”, 36(1), pp. 37–42.
]Search in Google Scholar
[
[20] Kalkamanov, S.A., Chygryn, R.M., 2003, “Metodika rascheta obtekaniya diskoobraznogo kryla potokom ideal’noj zhidkosti” [Method for calculating the flow of an ideal fluid around a disk-shaped wing], Open information and computer integrated technologies, National Aerospace University “Kharkiv Aviation Institute”, 21, pp. 63–66.
]Search in Google Scholar
[
[21] Kornienko, A.P., Ukrainets, E.O., Mokry, Yu.V., 2004, “Metodyka rozrakhunku aerodynamichnykh kharakterystyk systemy arochne krylo – shtovkhaiuchyi hvynt” [Method of calculating the aerodynamic characteristics of the system arched wing - pushing propeller], Issues of design and manufacture of aircraft structures, National Aerospace University “Kharkiv Aviation Institute”, 39(4), pp. 71–79.
]Search in Google Scholar
[
[22] Kornienko, A.P., 2005, “Eksperimental’nye issledovaniya haraktera obtekaniya izolirovannyh pryamogo i arochnogo kryl’ev” [Experimental studies of the nature of the flow of isolated straight and arched wings], Issues of design and manufacture of aircraft structures, National Aerospace University “Kharkiv Aviation Institute”, 42(3), pp. 118–123.
]Search in Google Scholar
[
[23] Kornienko, A.P., 2005 “Eksperimental’nye issledovaniya kartiny raspredeleniya davleniya po poverhnosti arochnogo kryla v sisteme ‘arochnoe krylo – tolkayushchij vozdushnyj vint’” [Experimental studies of the pattern of pressure distribution on the surface of the arched wing in the system “arched wing - pushing air screw”] Zbirnyk naukovykh prats KhUPS, 5(5), pp. 10–13.
]Search in Google Scholar
[
[24] Kornienko, A.P., Leontiev, A.B, Ukrainets, E. A., 2006, “Ocenka vliyaniya otnositel’nogo polozheniya vozdushnogo vinta na aerodinamicheskie harakteristiki kombinacii “arochnoe krylo – vozdushnyj vint”” [Evaluation of the influence of the relative position of the propeller on the aerodynamic characteristics of the combination “arched wing – propeller”], Information Processing Systems, Kharkiv. KhUPS, 4(53), pp. 87–94.
]Search in Google Scholar
[
[25] Kydushun, I.V., 2001, “Raritety amerikanskoj aviacii” [Rarities of American aviation], Moscow, ACT, pp. 112-147. http://loveread.ec/read_book.php?id=77533&p=22.
]Search in Google Scholar
[
[26] Ruzhitsky, E.I., 2000, “Amerikanskie samolety vertikal’nogo vzleta” [American vertical takeoff aircraft], Moscow, Astrel ACT. pp. 74–114. https://royallib.com/book/rugitskiy_evgeniy/amerikanskie_samoleti_vertikalnogo_vzleta.html
]Search in Google Scholar
[
[27] Gotsak, V.V., 2005, “Syntez metodu zburenykh potentsialiv ta metodu dyskretnykh vykhoriv dlia rozrakhunku neliniinykh nestatsionarnykh aerodynamichnykh kharakterystyk litakiv” [Synthesis of the perturbed potential method and the discrete vortex method for calculating nonlinear nonstationary aerodynamic characteristics of aircraft], Zbirnyk naukovykh prats KhUPS, Kharkiv, 3(3), pp. 29–31.
]Search in Google Scholar
[
[28] Radtsig, A.N., 2004, Eksperimental’naya gidroaeromekhanika [Experimental hydroaeromechanics], Moscow, MAI, p. 296.
]Search in Google Scholar
[
[29] Miranda, L.R. and Brennan, J.E., 1986, “Aerodynamic effects of wing tip mounted propellers and turbines”, AIAA 86(1802), pp. 221–228.10.2514/6.1986-1802
]Search in Google Scholar
[
[30] Vasin, I. S., 2010, “Issledovanie vliyaniya struj ot vozdushnyh vintov na aerodinamicheskie harakteristiki samoleta” [Study of the influence of jets from propellers on the aerodynamic characteristics of an aircraft], Scientific Bulletin MGTU GA, 151, pp. 39–43. https://cyberleninka.ru/article/n/issledovanie-vliyaniya-struy-ot-vozdushnyh-vintov-naaerodinamicheskie-harakteristiki-samoleta/viewer.
]Search in Google Scholar
[
[31] Radtsig, A.N., Semenchikov, N.V., 1992, Model’nyj eksperiment v aerodinamicheskih trubah [Model experiment in wind tunnels], Moscow, MAI, p. 65.
]Search in Google Scholar
[
[32] Zhuravlev, V.N., 2016, Aerodinamicheskij kompleks HAI - osnovnye etapy razvitiya i nauchnoj deyatel’nosti 1950–2010 [Aerodynamic complex KhAI – the main stages of development and scientific activity 1950–2010], National Aerospace University “Kharkiv Aviation Institute”, p. 156. http://aoleynik.info/aerodinamicheskij-kompleks-xai/.
]Search in Google Scholar
[
[33] Kravets, A.S., 1941, Harakteristiki vozdushnyh vintov [Propeller specifications], Moscow, State Publishing House of the Defense Industry, pp. 148–151.
]Search in Google Scholar
, 