Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin

• Autore: Marroquin J.
• Pubblicazione: Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985
• Descrizione fisica: 1 online resource (iii, 27 pages) : illustrations
• Soggetto topico: Aerothermodynamics; Hypersonic heat transfer; Aerodynamic heat transfer; Hypersonic speed; Wind tunnel tests
• Note generali: "DMS-DR-2524."; "March 1985."
• Nota di bibliografia: Includes bibliographical references (page 15).
• Altri titoli varianti: Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel
• Titolo autorizzato: Results of A M
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910709972703321
• Lo trovi qui: Univ. Federico II