Calculation of Compressible Potential Flow Past Slender Bodies of Revolution by an Integral Method

Calculation of Compressible Potential Flow Past Slender Bodies of Revolution by an Integral Method PDF Author: Milton M. Klein
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 60

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Book Description
An integral method, previously used to obtain compressible flow past two-dimensional shapes, is applied to the calculation of compressible potential flow past slender bodies of revolution. Good agreement of the resulting velocities on ellipsoids of revolution with those obtained by other methods was found. Flow-field conditions, in particular, local supersonic regions, are calculated and discussed. The free-stream Mach number beyond which a continuous potential-flow solution ceases to exist is found to be very close to 1.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 404

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464

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Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620

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Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462

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Technical Information Pilot

Technical Information Pilot PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 500

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Aeronautical Engineering Review

Aeronautical Engineering Review PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1456

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Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars

Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars PDF Author: Richard R. Heldenfels
Publisher:
ISBN:
Category : Box beams
Languages : en
Pages : 712

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Book Description
A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.