Author: George E. Kaattari
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
A Method for Predicting Pressures on Elliptic Cones at Supersonic Speeds
Author: George E. Kaattari
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
A Method for Predicting Pressures on Elliptic Cones at Supersonic Speeds
Author: George E. Kaattari
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 23
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 23
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
Book Description
Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. Kaattari
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Analytic Methods in Aircraft Aerodynamics
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 758
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 758
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Aerodynamics of Supersonic Lifting Bodies
Author: Martin C. Jischke
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 414
Book Description
This report describes a combined theoretical and experimental program of research in the aerodynamics of supersonic lifting bodies. Analytical perturbation techniques are used to study the supersonic flow past slightly elliptical cones, cones whose cross-sections deviate slightly but arbitrarily from that of a right circular cone, cones of small longitudinal curvature, and right circular cones undergoing small harmonic pitching and/or plunging motions. These studies all involve perturbations of the well-known solution for supersonic flow past a right circular cone. Closed-form analytical results are achieved through the use of an approximation that accurately predicts results over the entire range of the hypersonic similarity parameter. These results give hypersonic limiting solutions that agree well with other independent analyses and, at the same time, agree exactly with linearized theory in the linear theory limit. Comparisons with experiment, where possible, also show good agreement.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 414
Book Description
This report describes a combined theoretical and experimental program of research in the aerodynamics of supersonic lifting bodies. Analytical perturbation techniques are used to study the supersonic flow past slightly elliptical cones, cones whose cross-sections deviate slightly but arbitrarily from that of a right circular cone, cones of small longitudinal curvature, and right circular cones undergoing small harmonic pitching and/or plunging motions. These studies all involve perturbations of the well-known solution for supersonic flow past a right circular cone. Closed-form analytical results are achieved through the use of an approximation that accurately predicts results over the entire range of the hypersonic similarity parameter. These results give hypersonic limiting solutions that agree well with other independent analyses and, at the same time, agree exactly with linearized theory in the linear theory limit. Comparisons with experiment, where possible, also show good agreement.
A Semi-emperical Prediction Method for Pressures on the Windward Surface of Circular Cones at Incidence at High Supersonic and Hypersonic Speeds(M>3) by J.R.Collingbourne, L.F.Crabtree and W.J.Bartlett
Author: J.R. Collingbourne
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 15
Book Description
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 15
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