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1
Mission and sizing analysis for the Beta II two-stage-to-orbit vehicle by Nadell, Shari-Beth
Published 1992Call Number: Loading…
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2
Axisymmetric inlet minimum weight design method by Nadell, Shari-Beth
Published 1995Call Number: Loading…
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3
Minimum weight design of a generic axisymmetric inlet by Nadell, Shari-Beth
Published 1996Call Number: Loading…
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4
Minimum weight design of a generic axisymmetric inlet / by Nadell, Shari-Beth
Published 1996Call Number: Loading…Online Access
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5
A user's guide for the Differential Reduced Ejector/mixer Analysis "DREA" program version 1.0 / by De Chant, Lawrence J.
Published 1999Other Authors: “…Nadell, Shari-Beth…”
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Related Subjects
Supersonic inlets
Air intakes
Engine design
Finite element method
Structural design
Structural weight
Symmetry
Construction
Critical loading
Frames
High speed
Hypersonic planes
Loads (Forces)
Pressure distribution
Propulsion system configurations
Propulsion system performance
Reusable space vehicles
Systems analysis