R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel / / Renaldo V. Jenkins

• Record Nr.: UNINA9910709712803321
• Autore: Jenkins Renaldo V.
• Pubbl/distr/stampa: Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986
• Descrizione fisica: 1 online resource (111 pages) : illustrations
• Collana: NASA/TP ; ; 2565
• Soggetti: Airfoils; Reynolds number; Transonic wind tunnels; Mach number; Boundary layers; Aerofoils - Testing; Wall pressure (Aerodynamics); Boundary layer; Statistics.
• Lingua di pubblicazione: Inglese
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Note generali: Prepared at Langley Research Center.; "May 1986."
• Nota di bibliografia: Includes bibliographical references (pages 9-10).