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AGARD Advisory Report. Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification / AGARD Advisory Group (1997) / 978-92-8361-056-4
Titre de série : AGARD Advisory Report Titre : Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1997 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-321 Importance : 84 p. Présentation : schémas Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-056-4 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Wind tunnels Mass flowmeters Drag Calibrating Transferring Standards Test Nozzles Aircraft engines Viscosity Thrust meters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a multinational effort to reflect the state-of-the Art for the accurate measurement of massflow and thrust. The accurate measurements of these quantities is essential to the success of windtunnel tests supporting engine-airframe aerodynamic integration studies. Ist is concluded that the measurement og gaseous mass flows with +0.1% respectively. For thrust measurements, these values must typically be doubled. AGARD Advisory Report. Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1997 . - 84 p. : schémas ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-321) .
ISBN : 978-92-8361-056-4
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Wind tunnels Mass flowmeters Drag Calibrating Transferring Standards Test Nozzles Aircraft engines Viscosity Thrust meters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a multinational effort to reflect the state-of-the Art for the accurate measurement of massflow and thrust. The accurate measurements of these quantities is essential to the success of windtunnel tests supporting engine-airframe aerodynamic integration studies. Ist is concluded that the measurement og gaseous mass flows with +0.1% respectively. For thrust measurements, these values must typically be doubled. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2907 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
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