Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham

• Autore: Noonan Kevin W.
• Pubblicazione: [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
• Descrizione fisica: 1 online resource (82 pages) : chiefly illustrations
• Soggetto topico: Aerodynamic characteristics; Airfoils; Helicopters; Reynolds number; Wind tunnel tests; Aerofoils - Testing; Helicopters - Aerodynamics; Rotors (Helicopters) - Testing
• Persona (resp. second.): BinghamGene J.
• Note generali: Title from title screen (viewed on Aug. 16, 2016).; "September 1980."; "Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technology Laboratories"--Report documentation page.
• Nota di bibliografia: Includes bibliographical references (page 13).
• Titolo autorizzato: Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707473303321
• Lo trovi qui: Univ. Federico II