Titre de série :	AGARD Advisory Group
Titre :	Engine-airframe integration for rotorcraft
Type de document :	texte imprimé
Auteurs :	AGARD Lecture Series, Auteur
Editeur :	NATO - OTAN
Année de publication :	1986
Collection :	AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-148
Importance :	154 p.
Format :	21 x 30 cm.
Langues :	Anglais (eng)
Catégories :	Archives 8 AR-P.MARE
Tags :	Helicopters  Aircraft engines  Airframes  Gear drives
Index. décimale :	363.124 Risques dans les transports : Transports aérien et spatial
Résumé :	This lecture series will addres numerous engine airframe integration aspects relating to rotor wing aircraft. Various areas of engine airframe integration, including the impact of advanced engine design variable to specific propulsion subsystems, i.e. engine air inlets, will be discussed. Other propulsion sustem integration aspects such as engine/rotor/drive system torsional stability and transient response will be addressed. Additional areas considering this specification and qualification requirements of propulsion items will also be discussed.

AGARD Advisory Group. Engine-airframe integration for rotorcraft [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1986 . - 154 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-148) .
Langues : Anglais (eng)

Catégories :	Archives 8 AR-P.MARE
Tags :	Helicopters  Aircraft engines  Airframes  Gear drives
Index. décimale :	363.124 Risques dans les transports : Transports aérien et spatial
Résumé :	This lecture series will addres numerous engine airframe integration aspects relating to rotor wing aircraft. Various areas of engine airframe integration, including the impact of advanced engine design variable to specific propulsion subsystems, i.e. engine air inlets, will be discussed. Other propulsion sustem integration aspects such as engine/rotor/drive system torsional stability and transient response will be addressed. Additional areas considering this specification and qualification requirements of propulsion items will also be discussed.