Author: Milton M. Klein
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 60
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.
Calculation of Compressible Potential Flow Past Slender Bodies of Revolution by an Integral Method
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 404
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 404
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Book Description
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462
Book Description
Technical Information Pilot
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 500
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 500
Book Description
Aeronautical Engineering Review
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1456
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1456
Book Description
Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars
Author: Richard R. Heldenfels
Publisher:
ISBN:
Category : Box beams
Languages : en
Pages : 712
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.
Publisher:
ISBN:
Category : Box beams
Languages : en
Pages : 712
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.