Handbook of Supersonic Aerodynamics. Section 8. Bodies of Revolution

Handbook of Supersonic Aerodynamics. Section 8. Bodies of Revolution PDF Author: JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB.
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Languages : en
Pages : 365

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This section of the Handbook presents data on the aerodynamic characteristics of bodies of revolution for an angle-of-attack range of zero to almost ninety degrees throughout the supersonic and hypersonic flight regimes. Basic theories governing the pressure distributions on bodies of revolution and in their surrounding flow fields are discussed and evaluated. To provide a basis for the selection of theoretical methods to be used in specific calculation the reliability and accuracy of these theories are compared at different Mach and Reynolds numbers. Actual step-by-step development is omitted except where it is essential to an understanding of resultant expressions. In all cases, however, sources containing full derivations are referenced. To permit comparison or extension of the theoretical methods, experimentally-derived data in many instances are also presented. For those cases in which there is discrepancy between theory and experiment, empirical formulae are given together with the limiting values of the parameters within which the particular formula is valid. Techniques for incorporating the effects of skin friction and heat transfer (treated fully in Sections 13 and 14 of the Handbook) are also given.

Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: L.L. Cronvich
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Category :
Languages : en
Pages :

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Handbook of Supersonic Aerodynamics Section 8 Bodies of Revolution

Handbook of Supersonic Aerodynamics Section 8 Bodies of Revolution PDF Author:
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ISBN:
Category :
Languages : en
Pages : 366

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Handbook of Supersonic Aerodynamics: section 17. Dusts, nozzles and diffusers. section 18. Shock tubes. section 20. Wind tunnel instrumentation and operation

Handbook of Supersonic Aerodynamics: section 17. Dusts, nozzles and diffusers. section 18. Shock tubes. section 20. Wind tunnel instrumentation and operation PDF Author: Johns Hopkins University. Applied Physics Laboratory
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Category : Aerodynamics, Supersonic
Languages : en
Pages :

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Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642

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Handbook of Blunt-body Aerodynamics

Handbook of Blunt-body Aerodynamics PDF Author: John A. Darling
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Category : Aerodynamics
Languages : en
Pages : 154

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The report describes methods for quickly estimating the normal force and center of pressure of blunt free-fall shapes of l/d = 0.5 to 10 over a Mach number range of 0.4 to 2.5 and up to alpha = 90 degrees. Charts and equations presented in the report are from cited reference material and original sources. Methods based on slender-body theory tested on blunt shapes and modifying factors were developed where needed.

Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: Johns Hopkins University. Applied Physics Laboratory
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages :

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An Empirical Method for Determining Static Distributed Aerodynamic Loads on Axisymmetric Multistage Launch Vehicles

An Empirical Method for Determining Static Distributed Aerodynamic Loads on Axisymmetric Multistage Launch Vehicles PDF Author: Ralph John Muraca
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 104

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NASA technical note

NASA technical note PDF Author:
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Category : Aeronautics
Languages : en
Pages : 860

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NASA Technical Note

NASA Technical Note PDF Author: United States. National Aeronautics and Space Administration
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ISBN:
Category : Aeronautics
Languages : en
Pages :

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