High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By: Robert S. Jankovsky and Timothy D. Smith, Albert J. Pavli.
Contributors: Pavli, Albert J.; Smith, Timothy D.; NASA Glenn Research Center.
Series: NASA/TP -- 1999-208522; NASA technical paper -- 208522.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Number of pages: 51
Subjects: Aerodynamic load.; Boundary layer.; Combustion chambers.; Heat -- Transmission -- Measurement.; Nozzles.; Pressure -- Measurement.; Rocket engines.; Turbulence.
Other titles: High area ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
Notes: "June 1999."

"Performing organization report number E-11265"--Report documentation page.

Includes bibliographical references.

Prepared by National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field WU-632-1B-1B-00