Author: John V. RakichPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68
Book Description
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.
A Method of Characteristics for Steady Three-dimensional Supersonic Flow with Application to Inclined Bodies of Revolution
Author: John V. RakichPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68
Book Description
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.
Calculation of Nonlinear Conical Flows by the Method of Lines
Author: E. B. KlunkerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Book Description
A computational technique, called the method of lines, is developed for computing the flow field about conical configurations at incidence in a supersonic flow. The method, which makes use of the self-similarity property, is developed for the nonlinear flow equations. The method has proved to be an efficient and versatile procedure for constructing the numerical solutions to conical flow problems. It has been successful in computing the flow about circular and elliptic cones at conditions where small regions of supersonic cross flow develop and for the conical delta wings where the region of supersonic cross flow is extensive. The calculations made for circular and elliptic cones as well as for the compression side of various conical delta wings are in good agreement with experiment except in regions where viscous effects become important.
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Book Description
The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Theory and applications
Author: Chong-Wei ChuPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Book Description
NASA Technical Note
Author: NASA SP.
Author: Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. KaattariPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Author: