Hypervelocity impact induced disturbances on composite sandwich panel spacecraft structures
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISBN
-
9783816775553
- Maße
-
21 cm
- Umfang
-
IX, 228 S.
- Sprache
-
Englisch
- Anmerkungen
-
Ill., graph. Darst.
Zugl.: Melbourne, Univ., Diss., 2007
- Erschienen in
-
ε - Forschungsergebnisse aus der Kurzzeitdynamik ; H. Nr. 15
- Ereignis
-
Veröffentlichung
- (wo)
-
[Stuttgart]
- (wer)
-
[Fraunhofer-IRB-Verl.]
- (wann)
-
2008
- Urheber
-
Ryan, Shannon
- Inhaltsverzeichnis
- Rechteinformation
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Letzte Aktualisierung
-
11.06.2025, 13:52 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Ryan, Shannon
- [Fraunhofer-IRB-Verl.]
Entstanden
- 2008
Ähnliche Objekte (12)
Parametric study on dynamic responses of stiffened sandwich composite bridge deck panel
Durability assessment of sandwich panel construction
Thermoplastic composite sandwiches for structural helicopter applications
Principal Component Gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Maximum-variance gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Bending analysis of sandwich panel composite with a re-entrant lattice core using zig-zag theory
Fire behaviour of a Carbon/Nomex honeycomb sandwich composite used in aircraft interiors as ceiling panel
Time-Specific Disturbances in a Panel Data Stationarity Test
Time-Specific Disturbances in a Panel Data Stationarity Test
UHPC sandwich structures with composite coating under compressive load
Experimental Investigations of Compressed Sandwich Composite/Honeycomb Cylindrical Shells
Glass‐rigid foam composite for innovative concrete sandwich elements
Parametric study on dynamic responses of stiffened sandwich composite bridge deck panel
Durability assessment of sandwich panel construction
Thermoplastic composite sandwiches for structural helicopter applications
Principal Component Gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Maximum-variance gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Bending analysis of sandwich panel composite with a re-entrant lattice core using zig-zag theory
Fire behaviour of a Carbon/Nomex honeycomb sandwich composite used in aircraft interiors as ceiling panel
Time-Specific Disturbances in a Panel Data Stationarity Test
Time-Specific Disturbances in a Panel Data Stationarity Test
UHPC sandwich structures with composite coating under compressive load
Experimental Investigations of Compressed Sandwich Composite/Honeycomb Cylindrical Shells
Glass‐rigid foam composite for innovative concrete sandwich elements
Parametric study on dynamic responses of stiffened sandwich composite bridge deck panel
Durability assessment of sandwich panel construction
Thermoplastic composite sandwiches for structural helicopter applications
Principal Component Gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Maximum-variance gradiometer technique for removal of spacecraft-generated disturbances from magnetic field data
Bending analysis of sandwich panel composite with a re-entrant lattice core using zig-zag theory
Fire behaviour of a Carbon/Nomex honeycomb sandwich composite used in aircraft interiors as ceiling panel
Time-Specific Disturbances in a Panel Data Stationarity Test
Time-Specific Disturbances in a Panel Data Stationarity Test
UHPC sandwich structures with composite coating under compressive load
Experimental Investigations of Compressed Sandwich Composite/Honeycomb Cylindrical Shells