✦ LIBER ✦

Method for calculating the unsteady flow of an elliptical circulation-control airfoil

✍ Scribed by SUN, MAO; WANG, WEI

Book ID: 125481616
Publisher: American Institute of Aeronautics and Astronautics
Year: 1989
Tongue: English
Weight: 721 KB
Volume: 26
Category: Article
ISSN: 0021-8669
DOI: 10.2514/3.45860

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

PROJECTION METHODS FOR THE CALCULATION O

PROJECTION METHODS FOR THE CALCULATION OF INCOMPRESSIBLE UNSTEADY FLOWS

✍ Ni, Ming-Jiu; Komori, Satoru; Morley, Neil 📂 Article 📅 2003 🏛 Taylor and Francis Group 🌐 English ⚖ 1005 KB

An example of active circulation control

An example of active circulation control of the unsteady separated flow past a semi-infinite plate

✍ Cortelezzi, L.; Leonard, A.; Doyle, J. C. 📂 Article 📅 1994 🏛 Cambridge University Press 🌐 English ⚖ 499 KB

A Helmholtz pressure equation method for

A Helmholtz pressure equation method for the calculation of unsteady incompressibl eviscous flows

✍ Morgan Williams 📂 Article 📅 1992 🏛 John Wiley and Sons 🌐 English ⚖ 720 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 4th Flow Control Conference - Seattle, Washington (23 June 2008 - 26 June 2008)] 4th Flow Control Conference - Experimental Investigation Into a 10:1 Elliptical Airfoil with Circulation Control Augmentation for Rotorcraft Use

✍ Angle, Gerald; Kweder, Jonathan; Hubbell, Meagan; Smith, James; Wilhelm, Jay 📂 Article 📅 2008 🏛 American Institute of Aeronautics and Astronautics ⚖ 824 KB

Calculation of an unsteady moving-bounda

Calculation of an unsteady moving-boundary flow in a porous medium by the generalized method of integral relations

✍ R. A. Mustafaev 📂 Article 📅 2008 🏛 SP MAIK Nauka/Interperiodica 🌐 English ⚖ 134 KB

SUPERPOSITION TECHNIQUE FOR POTENTIAL FL

SUPERPOSITION TECHNIQUE FOR POTENTIAL FLOW AROUND AN AEROFOIL AND CONTROL OF THE CIRCULATION

✍ M. ADIIL YÜKSELEN 📂 Article 📅 1996 🏛 John Wiley and Sons 🌐 English ⚖ 353 KB

In this paper the superposition technique for a potential flow around an aerofoil is investigated in the complex plane. The control of the circulation around the aerofoil by satiseing the Kutta condition at the flow field points is described.