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Fluid mechanics / Drag divergence Mach number / Airfoil / Supercritical airfoil / Drag / Lift / Pressure coefficient / Camber / Mach number / Aerodynamics / Aerospace engineering / Fluid dynamics


MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive and
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Document Date: 2005-10-26 05:29:51


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Seine / Washington D.C. / London / Hamburg / New York / Santa Ana / /

Company

Mitsubishi / Bombardier / McDonnell Douglas / Airbus / Boeing / Raytheon / McGraw-Hill / /

Country

France / /

Facility

Stanford University / University Press / S. Ciornei Hamburg University of Applied Sciences Department / Hamburg University of Applied Sciences / /

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parameter accounting / literature search / /

Organization

North Atlantic Treaty Organization / Department of Automotive and Aeronautical Engineering / Hamburg University of Applied Sciences / Stanford University / S. Ciornei Hamburg University of Applied Sciences Department of Automotive and Aeronautical Engineering Berliner Tor / Department of Aeronautics and Astronautics / Institut für Luft / BAYAN / Stanford / /

Person

W EISSHAAR / /

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Position

The aircraft designer / /

Product

McDonnell Douglas DC-9 / BAC One-Eleven / Beriev Be-40 / McDonnell Douglas DC-10 / Dassault Falcon 20 / Tupolev Tu-204 / Douglas DC-8 / Boeing 767-200 / Lockheed Jetstar / swept wing / Airbus A300 / Airbus A310-300 / C-141 Starlifter / Bombardier Global Express / Lockheed C-5A MDD / Airbus A340-300 / Sud Aviation Caravelle / /

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Stanford University / /

Technology

data modeling / pdf / /

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http /

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