Airplane design 2 Preliminary configuration design and integration of the propulsion system

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Bibliographische Detailangaben
1. Verfasser:	Roskam, Jan (VerfasserIn)
Format:	UnknownFormat
Veröffentlicht:	Ottawa, Kan. Roskam Aviation and Engineering Corp. 2004
Ausgabe:	4. pr
Schlagworte:
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Titel	Jahr	Band
Airplane design 7 Determination of stability, control and performance characteristics: FAR and military requirements	2006	Pt. 7
Airplane design 8 Airplane cost estimation : design, development, manufacturing and operating	2006	Pt. 8
Airplane design 1 Preliminary sizing of airplanes	2005	Pt. 1
Airplane design 4 Layout design of landing gear and systems	2004	Pt. 4
Airplane design 2 Preliminary configuration design and integration of the propulsion system	2004	Pt. 2
Airplane design 6 Preliminary calculation of aerodynamic, thrust and power characteristics	2004	Pt. 6
Airplane design 5 Component weight estimation	2003	Pt. 5
Airplane design 3 Layout design of cockpit, fuselage, wing and empennage: cutaways and inboard profiles	2002	Pt. 3
Airplane Design Pt. 8 Airplane cost estimation: design, development, manufacturing and operating	1990	Pt. 8
Airplane Design Pt. 6 Preliminary calculation of aerodynamic, thrust and power characteristics	1987	Pt. 6
Airplane Design Pt. 3 Layout design of cockpit, fuselage, wing and empennage: cutaways and inboard profiles	1986	Pt. 3
Airplane Design Pt. 4 Layout design of landing gear and systems	1986	Pt. 4
Airplane Design Pt. 2 Preliminary configuration design and integration of the propulsion system	1985	Pt. 2
Airplane Design Pt. 5 Component weight estimation	1985	Pt. 5
Airplane Design Pt. 1 Preliminary sizing of airplanes	1985	Pt. 1