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26480

DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE

Article

Last updated: 04 Jan 2025

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Abstract

Dynamic stall constitutes a major limiting factor for helico-pter's forward speed. Calculations of rotor airloads and helicopter limiting speeds introducing the blade pitching oscillations effects, translate the real case into a reasonable analytical model. The present technique offers a reliable mean for calculating the rotor airloads with the unsteady effects. The method is extended to determine the limiting forward speed of helicopter.

DOI

10.21608/asat.1985.26480

Authors

First Name

E.

Last Name

TALAAT

MiddleName

-

Affiliation

Research Engineer-E.A.F., .Cairo, Egypt.

Email

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City

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Orcid

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First Name

M.

Last Name

KATARY

MiddleName

A.

Affiliation

Department of Aeronautics, Millitary Technical College, Cairo, Egypt.

Email

-

City

-

Orcid

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Volume

1

Article Issue

A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO

Related Issue

4758

Issue Date

1985-05-01

Receive Date

2019-02-04

Publish Date

1985-05-01

Page Start

255

Page End

265

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 1_Issue A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO_Pages 255-265.pdf

PDF . 2.1MB

Link

https://asat.journals.ekb.eg/article_26480.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26480

Order

20

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE

Details

Type

Article

Created At

22 Jan 2023