Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis
By: Timothy D. Smith ... [et al.].
Contributors: Smith, Timothy D.; Lewis Research Center.
Series: NASA/TM -- 1998-206632.; NASA technical memorandum -- 206632.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Combined cycle power generation.; Rocket engines.; Specific impulse.; Regression analysis.; Experiment design.; Rocket nozzles.; K-omega turbulence model.
Notes: Shipping list no.: 99-0265-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.