INFORMAZIONI SU QUESTO ARTICOLO

Cita

[1] Okninski, A., 2015, “An optimization of sounding rockets for microgravity research”, 66th International Astronautical Congress, Jerusalem, IAC-15, A2, 5, 10, x30167. Search in Google Scholar

[2] Walczewski, J., 1982, Polish sounding rocket program (Polskie rakiety badawcze), Wydawnictwa Komunikacji i Łączności, Warsaw. Search in Google Scholar

[3] Wiśniowski, W. and Wolański, P., 2014, „Rola Instytutu Lotnictwa w badaniach kosmicznych” (Institute of Aviation Activities in the field of space research), Prace Instytutu Lotnictwa (Transactions of the Institute of Aviation), No. 234, pp. 9-16.10.5604/05096669.1106721 Search in Google Scholar

[4] Grzegorzewski, J., 1992, „Prace Instytutu Lotnictwa w dziedzinie techniki rakietowej” (Work of the Institute of Aviation Activities in the field of space research), Prace Instytutu Lotnictwa (Transactions of the Institute of Aviation), No. 131. Search in Google Scholar

[5] Kaźmierski, J., Krawczyk, Z. and Nowak, K., 1997, „Technologia rakietowa i kosmiczna w Instytucie Lotnictwa” (Rocket and Space technology in the Institute of Aviation), Prace Instytutu Lotnictwa (Transactions of the Institute of Aviation), No. 151. Search in Google Scholar

[6] Lewandowski, R., 1967, „Obciążenie aerodynamiczne niekierowanych rakiet balistycznych” (Aerodynamic loads of non-guided ballistic rockets), Prace Instytutu Lotnictwa (Transactions of the Institute of Aviation), No. 31, pp. 30-44. Search in Google Scholar

[7] Kurow, W. and Dolzanski, J., 1964, Solid propellant rocket missile design, Military University of Technology Publisher, Warsaw. Search in Google Scholar

[8] Lewandowski, R., 1968, „Wpływ czynników zakłócających na ruch niekierowanej rakiety meteorologicznej“ (Influence of the disturbances on the non-guided mereology rocket flight), Prace Instytutu Lotnictwa (Transactions of the Institute of Aviation), No. 36, pp. 3-15. Search in Google Scholar

[9] Lopez, D., Domınguez, D. and Gonzalo, J., 2013, „Impact of turbulence modelling on external supersonic flow field simulations in rocket aerodynamics“, International Journal of Computational Fluid Dynamics, Vol. 27, Nos. 8-10, pp. 332–341.10.1080/10618562.2013.867951 Search in Google Scholar

[10] Rasuo, B. and Bengin, A., 2015, “Aerodynamic shape optimization of guided missile based on wind tunnel testing and CFD simulation“, Thermal Scienc, (00), pp.184-184. Search in Google Scholar

[11] Ocokolijić, G. and Rasuo, B., 2012, “Testing an Anti Tank Missile Model with Jet Simulation in the T-35 Subsonic Wind Tunnel“, Scientific Technical Review, No. 3-4(62), pp.14-20 Search in Google Scholar

[12] Bryson, H., Sültrop, H.P., Buchanan, G., Hann, C.E., Snowdon, M., Rao, A., Slee, A., Fanning, K., Wright, D., McVicar, J., Clark, B., Harris, G., Chen, X.Q., 2016, “Vertical Wind Tunnel for Prediction of Rocket Flight Dynamics“, Aerospace, No. 3(10).10.3390/aerospace3020010 Search in Google Scholar

[13] Ellis, S., 2017, “SLS Shocked During Wind Tunnel Testing to Better Understand Rocket’s Transonic Behavior“, NASA website, https://www.nasa.gov/feature/langley/sls-shocked-duringwind-tunnel-testing-to-better-understand-rocket-s-transonic-behavior Search in Google Scholar

[14] Marroquin, J. and Lemoine, P., 1992, “RESULTS OF WIND TUNNEL TESTS OF AN ASRM CONFIGURED 0.03 SCALE SPACE SHUTTLE INTEGRATED VEHICLE MODEL (47-OTS) IN THE AEDC 16-FOOT TRANSONIC WIND TUNNEL (IA613A), Space Shuttle aerothermodynamic data report“, DMS_DR-2548 NASA-CR-185, No. 696. Search in Google Scholar

[15] “Aerodynamics Research Laboratory website”, http://cntpolska.pl/zespol-aerodynamiki/laboratorium-aerodynamiki-stosowanej/?lang=en, access: 2018.01.19. Search in Google Scholar

[16] Adrian, R., 2005, J., “Twenty Years of Particle Image Velocimetry“, Experiments in Fluids, No. 39, pp. 159-169.10.1007/s00348-005-0991-7 Search in Google Scholar

[17] Stryczniewicz, W., 2012, “Development of Particle Image Velocimetry Algorithm“, Problems of Mechatronics, No. 9, pp. 41-54. Search in Google Scholar

[18] Surmacz, K., Ruchała, P. and Stryczniewicz, W., 2015, “Wind tunnel tests of the development and demise of Vortex Ring State of the rotor“, Advances in Mechanics: Theoretical, Computational and Interdisciplinary Issues, Proceedings of the 3rd Polish Congress of Mechanics (PCM) and 21st International Conference on Computer Methods in Mechanics (CMM), CRC Press, Gdansk, pp. 8-11.10.1201/b20057-118 Search in Google Scholar

[19] Dziopa, Z., 2007, Mechanika lotu (Flight mechanics), Wydawnictwo Politechniki Świętokrzyskiej, Kielce. Search in Google Scholar

[20] Fleeman, E., L., 2001, Tactical Missile Design, AIAA Education Series, American Institute of Aeronautics and Astronautics, Reston, USA. Search in Google Scholar

[21] Barrowman, J., S. and Barrowman, J., A., 1966, “The Theoretical Prediction of the Center of Pressure”, NARAM-8 R&D Project, from the Apogee Components web site: www.ApogeeRockets.com Search in Google Scholar

[22] Matyszewski, J., 2014, „Rozwój metod obliczeniowych do symulacji trajektorii lotu rakiet” (Development of rocket flight simulation methods), Prace Instytutu Lotnictwa (American Institute of Aeronautics and Astronautics), No. 1(234), pp. 90-103.10.5604/05096669.1106840 Search in Google Scholar

[23] Cieśliński, D., 2017, “Precise determination of static margins for unguided sounding rockets”, presentation and conference paper, 66th IAC, IAC-15,E2,1,4,x30641, Jerusalem. Search in Google Scholar

eISSN:
2545-2835
Lingua:
Inglese
Frequenza di pubblicazione:
4 volte all'anno
Argomenti della rivista:
Engineering, Introductions and Overviews, other, Geosciences, Materials Sciences, Physics