Propellant Vaporization as a Design Criterion for Rocket-engine Combustion Chambers PDF Download
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Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 64
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Book Description
Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 64
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Book Description
Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 68
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Book Description
Author: Marcus F. Heidmann
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 806
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Book Description
Author: Jack Norman Nielsen
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 682
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Book Description
Tables are presented containing 69,000 values of a set of characteristic functions which first arose in problems of supersonic wing-body interference. The tables are useful in problems of supersonic flow involving aerodynamic shapes which are wholly or in part quasi-cylinders of nearly circular cross section. A number of uses are described in the aerodynamics of bodies alone, body-body or shock-body interference, wing-body interference, the vortex-panel interference. Three illustrative examples are worked out in detail. First, the pressure field due to fuselage indentation is calculated and presented in a form independent of Mach number. Secondly, the tables are applied to a problem involving a previously unpublished solution to the Navier-Stokes equations; namely, the boundary-layer profiles of a circular cylinder moved impulsively with a constant axial force in a viscous incompressible fluid. In the final example, the wave drag of corrugated circular cylinders is calculated as a function of the number of corrugations and their wave length. Several nonaerodynamic applications are pointed out in the fields of acoustics and heat conduction. Generally speaking, the tables are applicable to boundary-value problems of the second kind involving the wave equation in three dimensions with approximately circular cylindrical boundaries or involving the unsteady heat-conduction equation in two space dimensions with nearly circular boundaries.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 370
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 420
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Book Description
Author: Vigor Young
Publisher: AIAA
ISBN: 9781600864186
Category : Liquid propellant rockets
Languages : en
Pages : 606
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Book Description
Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42
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Book Description
