Aerodynamic principles of the supersonic guide surface parachute:
The location of shock waves, the pressure distribution and the mass flow, which are significant for the functioning of a parachute in supersonic flow, are being discussed and some advantageous conditions are postulated. Wind tunnel studies are described in which the validity of the assumptions has b...
Gespeichert in:
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| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Minneapolis, Minn.
University of Minnesota, Institute of Technology, Dept. of Aeronautics and Engineering Mechanics
[1964?]
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| Schlagworte: | |
| Zusammenfassung: | The location of shock waves, the pressure distribution and the mass flow, which are significant for the functioning of a parachute in supersonic flow, are being discussed and some advantageous conditions are postulated. Wind tunnel studies are described in which the validity of the assumptions has been checked by means of models of a modified guide surface canopy combined with a shock producing cone. A configuration was found according to which 10-centimeter textile models function satisfactorily up to Mach numbers of 4.5. The results of further supersonic wind tunnel tests are shown in which a 1.2 meter supersonic guide surface parachute, built in accordance with the established aerodynamic parameters, functioned satisfactorily. This parachute collapsed due to structural weakness at a Mach number of 2.8 after being exposed to supersonic flow for approximately 90 minutes |
| Beschreibung: | "Presented at the WGLR-DGRR-Tagung, 14-18 September 1964, West Berlin, Germany"--T.p. - This work is part of the library's "Parachute History Collection" donated by the Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Flugsystemtechnik through the American Institute of Aeronautics and Astronautics Deceleration Systems Technical Committee Includes bibliographical references |
| Beschreibung: | 15, [21] S. ill. 28 cm |
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| 100 | 1 | |a Heinrich, Helmut G. |d 1910-1979 |e Verfasser |0 (DE-588)1028215746 |4 aut | |
| 245 | 1 | 0 | |a Aerodynamic principles of the supersonic guide surface parachute |c by Helmut G. Heinrich |
| 264 | 1 | |a Minneapolis, Minn. |b University of Minnesota, Institute of Technology, Dept. of Aeronautics and Engineering Mechanics |c [1964?] | |
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| 500 | |a "Presented at the WGLR-DGRR-Tagung, 14-18 September 1964, West Berlin, Germany"--T.p. - This work is part of the library's "Parachute History Collection" donated by the Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Flugsystemtechnik through the American Institute of Aeronautics and Astronautics Deceleration Systems Technical Committee | ||
| 500 | |a Includes bibliographical references | ||
| 520 | |a The location of shock waves, the pressure distribution and the mass flow, which are significant for the functioning of a parachute in supersonic flow, are being discussed and some advantageous conditions are postulated. Wind tunnel studies are described in which the validity of the assumptions has been checked by means of models of a modified guide surface canopy combined with a shock producing cone. A configuration was found according to which 10-centimeter textile models function satisfactorily up to Mach numbers of 4.5. The results of further supersonic wind tunnel tests are shown in which a 1.2 meter supersonic guide surface parachute, built in accordance with the established aerodynamic parameters, functioned satisfactorily. This parachute collapsed due to structural weakness at a Mach number of 2.8 after being exposed to supersonic flow for approximately 90 minutes | ||
| 650 | 4 | |a Parachutes / Aerodynamics / Congresses | |
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Datensatz im Suchindex
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| author | Heinrich, Helmut G. 1910-1979 |
| author_GND | (DE-588)1028215746 |
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| physical | 15, [21] S. ill. 28 cm |
| publishDate | 1964 |
| publishDateSearch | 1964 |
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| publisher | University of Minnesota, Institute of Technology, Dept. of Aeronautics and Engineering Mechanics |
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| spelling | Heinrich, Helmut G. 1910-1979 Verfasser (DE-588)1028215746 aut Aerodynamic principles of the supersonic guide surface parachute by Helmut G. Heinrich Minneapolis, Minn. University of Minnesota, Institute of Technology, Dept. of Aeronautics and Engineering Mechanics [1964?] 15, [21] S. ill. 28 cm txt rdacontent n rdamedia nc rdacarrier "Presented at the WGLR-DGRR-Tagung, 14-18 September 1964, West Berlin, Germany"--T.p. - This work is part of the library's "Parachute History Collection" donated by the Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Flugsystemtechnik through the American Institute of Aeronautics and Astronautics Deceleration Systems Technical Committee Includes bibliographical references The location of shock waves, the pressure distribution and the mass flow, which are significant for the functioning of a parachute in supersonic flow, are being discussed and some advantageous conditions are postulated. Wind tunnel studies are described in which the validity of the assumptions has been checked by means of models of a modified guide surface canopy combined with a shock producing cone. A configuration was found according to which 10-centimeter textile models function satisfactorily up to Mach numbers of 4.5. The results of further supersonic wind tunnel tests are shown in which a 1.2 meter supersonic guide surface parachute, built in accordance with the established aerodynamic parameters, functioned satisfactorily. This parachute collapsed due to structural weakness at a Mach number of 2.8 after being exposed to supersonic flow for approximately 90 minutes Parachutes / Aerodynamics / Congresses Parachutes / Testing / Congresses Parachutes / Aerodynamics fast Parachutes / Testing fast (DE-588)1071861417 Konferenzschrift gnd-content |
| spellingShingle | Heinrich, Helmut G. 1910-1979 Aerodynamic principles of the supersonic guide surface parachute Parachutes / Aerodynamics / Congresses Parachutes / Testing / Congresses Parachutes / Aerodynamics fast Parachutes / Testing fast |
| subject_GND | (DE-588)1071861417 |
| title | Aerodynamic principles of the supersonic guide surface parachute |
| title_auth | Aerodynamic principles of the supersonic guide surface parachute |
| title_exact_search | Aerodynamic principles of the supersonic guide surface parachute |
| title_full | Aerodynamic principles of the supersonic guide surface parachute by Helmut G. Heinrich |
| title_fullStr | Aerodynamic principles of the supersonic guide surface parachute by Helmut G. Heinrich |
| title_full_unstemmed | Aerodynamic principles of the supersonic guide surface parachute by Helmut G. Heinrich |
| title_short | Aerodynamic principles of the supersonic guide surface parachute |
| title_sort | aerodynamic principles of the supersonic guide surface parachute |
| topic | Parachutes / Aerodynamics / Congresses Parachutes / Testing / Congresses Parachutes / Aerodynamics fast Parachutes / Testing fast |
| topic_facet | Parachutes / Aerodynamics / Congresses Parachutes / Testing / Congresses Parachutes / Aerodynamics Parachutes / Testing Konferenzschrift |
| work_keys_str_mv | AT heinrichhelmutg aerodynamicprinciplesofthesupersonicguidesurfaceparachute |