Low Aspect-Ratio Wings for Wing-Ships

Antonino Filippone; M. Selig

Low Aspect-Ratio Wings for Wing-Ships

Antonino Filippone, M. Selig

University of Illinois

Research output: Chapter in Book/Report/Conference proceeding › Article in proceedings › Research › peer-review

Abstract

Flying on ground poses technical and aerodynamical challenges. The requirements for compactness, efficiency, manouverability, off-design operation,open new areas of investigations in the fieldof aerodynamic analysis and design. A review ofthe characteristics of low-aspect ratio wings, in- and out of ground, is presented. It is shownthat the performance of such wings is generally inferior to that of slender wings, although in ground placement can yield substantial improvements in the aerodynamic efficiency.

Original language	English
Title of host publication	Low Aspect-Ratio Wings for Wing-Ships
Place of Publication	Washington
Publisher	AIAA
Publication date	1998
Publication status	Published - 1998
Event	36th Aerospace Sciences Meeting - Reno, United States Duration: 12 Jan 1998 → 15 Jan 1998

Conference

Conference	36th Aerospace Sciences Meeting
Country/Territory	United States
City	Reno
Period	12/01/1998 → 15/01/1998

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title = "Low Aspect-Ratio Wings for Wing-Ships",

abstract = "Flying on ground poses technical and aerodynamical challenges. The requirements for compactness, efficiency, manouverability, off-design operation,open new areas of investigations in the fieldof aerodynamic analysis and design. A review ofthe characteristics of low-aspect ratio wings, in- and out of ground, is presented. It is shownthat the performance of such wings is generally inferior to that of slender wings, although in ground placement can yield substantial improvements in the aerodynamic efficiency.",

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AB - Flying on ground poses technical and aerodynamical challenges. The requirements for compactness, efficiency, manouverability, off-design operation,open new areas of investigations in the fieldof aerodynamic analysis and design. A review ofthe characteristics of low-aspect ratio wings, in- and out of ground, is presented. It is shownthat the performance of such wings is generally inferior to that of slender wings, although in ground placement can yield substantial improvements in the aerodynamic efficiency.

M3 - Article in proceedings

BT - Low Aspect-Ratio Wings for Wing-Ships

PB - AIAA

CY - Washington

T2 - 36th Aerospace Sciences Meeting

Y2 - 12 January 1998 through 15 January 1998

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