Zitieren

[1] Figat, Marcin., Galiński, Cezary. and Kwiek, Agnieszka. “Modular Aeroplane System. A Concept and Initial Investigation.” Proceeding of ICAS 2012 Conference, Brisbane, paper number ICAS 2012-1.3.2, paper no ICAS 2012-1.3.2 (2012). Search in Google Scholar

[2] Figat, Marcin. and Kwiek, Agnieszka. “Aerodynamic and Static Stability Investigation into Aircraft Coupled System to Suborbital Space Flights.” Aircraft Engineering and Aerospace Technology Vol. 93 No. 2 (2021): pp. 275–283. DOI 10.1108/AeAt-05-2020-0085. Open DOISearch in Google Scholar

[3] Galiński, Cezary., Goetzendorf-Grabowski, Tomasz., Mieszalski, Dawid. and Stefanek, Łukasz. “A Concept of two-Staged Spaceplane for Suborbital tourism.” Transactions of the Institute of Aviation Vol. 191 No. 4 (2007): pp. 33–42. Search in Google Scholar

[4] Antuñano, Melchor., Baisden, Denise., Davis, Jeffrey., Hastings, John., Jennings, Richard., Jones, David, Jordan, Jon, Mohler, Stanley., Ruehle, Charles., Salazar, Guillermo., Silberman, Warren., Scarpa, Phillip., Tilton, Frederick. and Whinnery, James. “Guidance for Medical Screening of Commercial Aerospace Passengers.” FAA report DOT/FAA/AM-06/1 (2006): Available at https://libraryonline.erau.edu/online-full-text/faa-aviation-medicine-reports/AM06-01.pdf (accessed on 10.01.2021). Search in Google Scholar

[5] Galiński, Cezary. and Goraj, Zdobysław. “Experimental and Numerical results Obtained for A Scaled RPV and A Full Size Aircraft.” Aircraft Engineering and Aerospace Technology Vol. 76 No. 3 (2004): pp. 305–313. DOI 10.1108/00022660410536041. Open DOISearch in Google Scholar

[6] Kimberlin, Ralph. Flight Testing of Fixed Wing Aircraft. American Institute of Aeronautics and Astronautics, Reston, VA (2003).10.2514/4.861840 Search in Google Scholar

[7] Chambers, Joseph. Modeling Flight. The Role of Dynamically Scaled Free-Flight Models in Support on NASA’s Aerospace Programs. U.S. Government Printing Office, Washington DC (2009). Search in Google Scholar

[8] Galiński, Cezary., Bartkiewicz, Piotr., Hajduk, Jarosław. and Lamers, Piotr. “Results of the J-5 Marco Dynamic Similar Model Flight Tests Program.” SAE Paper No. 975551, 1997 World Aviation Congress, 1316.10.1997, Anaheim, CA (1997).10.2514/6.1997-5551 Search in Google Scholar

[9] Wolowicz, Chester., Bowman, James Jr. and Gilbert, William. Similitude Requirements and Scaling Relationships as Applied to Model Testing.” NASA Technical Paper 1436. Search in Google Scholar

[10] SDSA – Simulation and Dynamic Stability analysis, Warsaw University of Technology, Available at www.meil.pw.edu.pl/add/ADD/teaching/Software/SDSA (accessed on 16.12.2021). Search in Google Scholar

[11] Goetzendorf-Grabowski, Tomasz., Marcinkiewicz, Ewa. and Galiński, Cezary. “Comparison of Traditionally Calculated Stability Characteristics with Flight Test Data of PW-6U sailplane.” Proceedings of the CEAS Conference, pp. 536–543. Linköping, Sweden, 15–19.09.2013. Linköping University Electronic Press, Linköping (2013). Search in Google Scholar

[12] Goetzendorf-Grabowski, Tomasz. and Antoniewski, Tomasz. “Three Surface Aircraft (TSA) Configuration – Flying Qualities Evaluation.” Aircraft Engineering and Aerospace Technology, Vol. 88 No. 2 (2016): pp. 277–284. DOI 10.1108/AEAt-02-2015-0055. Search in Google Scholar

[13] Mieloszyk, Jacek., Tarnowski, Andrzej., Tomaszewski, Adam. and Goetzendorf-Grabowski, Tomasz. “Validation of Flight Dynamic Stability Optimization Constraints with Flight tests.” Aerospace Science and Technology Vol. 106, (2020): DOI 10.1016/j.ast.2020.106193. Open DOISearch in Google Scholar

[14] Kwiek, Agnieszka., Galiński, Cezary., Bogdański, Krzysztof., Hajduk, Jarosław. and Tarnowski, Andrzej. “Results of Simulation and Scaled Flight Tests Performed on A Rocket-Plane at High Angles of Attack.” Aircraft Engineering and Aerospace Technology Vol. 93 No. 9, (2021): pp. 1445–1459. DOI 10.1108/AEAT-11-2020-0276. Open DOISearch in Google Scholar

[15] Galiński, Cezary. and Hajduk, Jarosław. “Assumptions of the Joined Wing Flying Model Programme.” Transactions Of The Institute of Aviation Vol. 238 No. 1 (2015): pp. 7–21. Search in Google Scholar

[16] Jouannet, Christopher., Berry, Patrick., Melin, Tomas., Amadori, Kristian., Lundström, David. and Staack, Ingo., “Subscale Flight Testing used in Conceptual Design.” Aircraft Engineering and Aerospace Technology Vol. 84 No. 3 (2012): pp. 192–199. DOI 10.1108/00022661211222058. Open DOISearch in Google Scholar

[17] Lundström, David., Sobron, Alejandro., Krus, Petter., Jouannet, Christopher., Gil Annes da Silva, R. “Subscale Flight Testing Of A Generic Fighter Aircraft.” 30th International Congress Of Aeronautical Sciences 25–30 Spetember 2016, Daejeon, Korea, paper No 2016_0390 (2016). Search in Google Scholar

[18] Yanagihara, Masaaki. and Munenaga, Takao. “High Speed Flight Demonstration Project”, 24th International Congress of Aeronautical Sciences, 29 August–3 September 2004, Yokohama, Japan, Paper No ICAS 2004-7.1.1 (I.L.) (2004). Search in Google Scholar

[19] Goraj, Zdobysław., Malinowski, Marek. and Frydrychewicz, Andrzej. “Design of Novel Aerial Jet Target.” Aircraft Engineering and Aerospace Technology Vol. 89 No. 4 (2017): pp. 511–519. DOI 10.1108/AEAT-10-2016-0174. Search in Google Scholar

[20] Banks Daniel. and Fisher David. “Aft-End Flow of a Large-Scale Lifting Body During Free-Flight Test.” NASA/TM-2006-213681 (2006). Search in Google Scholar

[21] Croom, Mark., Kenney, Holly., Murri, Daniel. and Lawson, Kenneth. “Research on the F/A-18e/F Using a 22%-Dynamically-Scaled Drop model.” AIAA Atmospheric Flight Mechanics Conference and Exhibition, 14–17 August 2000, Denver, Colorado (2000).10.2514/6.2000-3913 Search in Google Scholar

[22] Homan, D.J. Denison D.E. and Elchett, K.C. “Orbiter/Shuttle Carrier Aircraft Separation: Wind tunnel, Simulation, and Flight Test Overview and results.” NASA Technical Memorandum 58223 (1980). Search in Google Scholar

[23] Klein, Vladislav. and Noderer Keith. “Aerodynamic Parameters of the X-31 Drop Model Estimated from Flight-Data at High Angles of Attack.” Guidance, Navigation and Control Conference 10–12.08.1992, Hilton Head Island, SC, U.S.A., AIAA-92-4357CP (1992).10.2514/6.1992-4357 Search in Google Scholar

[24] Iliff, Kenneth., Maine, Richard. and Shafer, Mary. “Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8-Scale F-15 Airplane Model Obtained from Flight Test.” NASA Technical Note TN D-8136 (1976). Search in Google Scholar

[25] Lux Jessica. and Burkes Darryl. “Hyper-X (X-43A) Flight Test Range Operations Overview.” NASA/TM-2008-214626 (2008). Search in Google Scholar

[26] NASA. https://www.nasa.gov/exploration/commercial/crew/snc_captivecarry.html (accessed on 12.01.2022). Search in Google Scholar

[27] Evans, Carol. Orion Capsule Parachute Assembly System (CPAS) Airdrop Test Program Techniques, Challenges, and Solutions. AIAA Aviation and Aeronautics Forum, Dallas, TX (2019).10.2514/6.2019-3023 Search in Google Scholar

[28] Honda Masahisa. and Yoshida Kenji. “D-SeND#2 Flight Demonstration for Low Sonic Boom Design Technology.” 2014, 29th International Congress of Aeronautical Sciences, 7–12 September 2014, St. Petersburg, Russia, Paper No ICAS2014_0505 (2014) Search in Google Scholar

[29] Grossnick, Roy. Kite Balloons to Airship: the Navy’s Lighter than Air Experience. Published by the Deputy Chief of Naval Operations (Air Warfare) and the Commander, Naval Air System Command, Washington D.C. (1987). Search in Google Scholar

[30] Analytical Methods, INC., MGAERO user’s manual Version 3.1.4., Redmond, Washington USA, 1990-2001 Search in Google Scholar

[31] Corda, Stephen. and Vachon, Michael. “Design and Flight Evaluation of a New Force-Based Flow Angle Probe.” NASA Technical Memorandum NASA/TM-2006-213673 (2006). Search in Google Scholar

[32] Bennett, Donald. “Evaluation of Hemispherical Head Flow Direction Sensor for Inlet Duct Measurements.” NASA TMX-3232, (1975): Available at: www.nasa.gov/centers/dryden/pdf/87861main_H-862.pdf (accessed 10.01.2022). Search in Google Scholar

[33] Gonzalez, Jose. and Arrington, Allen. “Five-Hole Flow Angle Probe Calibration for the NASA glenn Icing Research Tunnel.” NASA/Cr-1999-202330 (1996). Available at: https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990047776.pdf (accessed 10.01.2022). Search in Google Scholar

eISSN:
2545-2835
Sprache:
Englisch
Zeitrahmen der Veröffentlichung:
4 Hefte pro Jahr
Fachgebiete der Zeitschrift:
Technik, Einführungen und Gesamtdarstellungen, andere, Geowissenschaften, Materialwissenschaft, Physik