Optimization of the twist distribution using an adaptive airfoil

R. L. Roglin; S. V. Hanagud; D. A. Peters; Aditi Chattopadhyay

Optimization of the twist distribution using an adaptive airfoil

R. L. Roglin, S. V. Hanagud, D. A. Peters, Aditi Chattopadhyay

Mechanical and Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

This paper presents a review of the equations necessary to solve the aeroelastic problem of a rotating airfoil. These equation form the basis for a study to determine the spanwise length of a control surface. The purpose of this control surface is to act as the primary mechanism for lift generation replacing the conventional method of altering the pitch angle of a rigid blade.

Original language	English (US)
Title of host publication	Annual Forum Proceedings - American Helicopter Society
Publisher	American Helicopter Soc
Pages	957-964
Number of pages	8
Volume	2
State	Published - 1995
Event	Proceedings of the 1995 51st Annual Forum. Part 1 (of 3) - Fort Worth, TX, USA Duration: May 9 1995 → May 11 1995

Other

Other	Proceedings of the 1995 51st Annual Forum. Part 1 (of 3)
City	Fort Worth, TX, USA
Period	5/9/95 → 5/11/95

ASJC Scopus subject areas

Aerospace Engineering
Transportation

Cite this

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title = "Optimization of the twist distribution using an adaptive airfoil",

abstract = "This paper presents a review of the equations necessary to solve the aeroelastic problem of a rotating airfoil. These equation form the basis for a study to determine the spanwise length of a control surface. The purpose of this control surface is to act as the primary mechanism for lift generation replacing the conventional method of altering the pitch angle of a rigid blade.",

author = "Roglin, {R. L.} and Hanagud, {S. V.} and Peters, {D. A.} and Aditi Chattopadhyay",

year = "1995",

language = "English (US)",

volume = "2",

pages = "957--964",

booktitle = "Annual Forum Proceedings - American Helicopter Society",

publisher = "American Helicopter Soc",

note = "Proceedings of the 1995 51st Annual Forum. Part 1 (of 3) ; Conference date: 09-05-1995 Through 11-05-1995",

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T1 - Optimization of the twist distribution using an adaptive airfoil

AU - Roglin, R. L.

AU - Hanagud, S. V.

AU - Peters, D. A.

AU - Chattopadhyay, Aditi

PY - 1995

Y1 - 1995

N2 - This paper presents a review of the equations necessary to solve the aeroelastic problem of a rotating airfoil. These equation form the basis for a study to determine the spanwise length of a control surface. The purpose of this control surface is to act as the primary mechanism for lift generation replacing the conventional method of altering the pitch angle of a rigid blade.

AB - This paper presents a review of the equations necessary to solve the aeroelastic problem of a rotating airfoil. These equation form the basis for a study to determine the spanwise length of a control surface. The purpose of this control surface is to act as the primary mechanism for lift generation replacing the conventional method of altering the pitch angle of a rigid blade.

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UR - http://www.scopus.com/inward/citedby.url?scp=0029454913&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0029454913

VL - 2

SP - 957

EP - 964

BT - Annual Forum Proceedings - American Helicopter Society

PB - American Helicopter Soc

T2 - Proceedings of the 1995 51st Annual Forum. Part 1 (of 3)

Y2 - 9 May 1995 through 11 May 1995

ER -

Optimization of the twist distribution using an adaptive airfoil

Abstract

Other

ASJC Scopus subject areas

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