Research Catalog

Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis

Title
Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis [microform] / Timothy D. Smith ... [et al.].
Publication
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]

Details

Additional Authors
  • Smith, Timothy D.
  • Lewis Research Center.
Description
1 v.
Series Statement
NASA/TM ; 1998-206632
Uniform Title
NASA technical memorandum ; 206632.
Subject
  • Combined cycle power generation
  • Rocket engines
  • Specific impulse
  • Regression analysis
  • Experiment design
  • Rocket nozzles
  • K-omega turbulence model
Note
  • Shipping list no.: 99-0265-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:206632
OCLC
marcive41027837
Title
Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis [microform] / Timothy D. Smith ... [et al.].
Imprint
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
Series
NASA/TM ; 1998-206632
NASA technical memorandum ; 206632.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Added Author
Smith, Timothy D.
Lewis Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:206632
Research Call Number
READEX Microfiche NAS 1.15:206632
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