Author: George E. Kaattari
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Estimation of Shock Layer Thickness and Pressure Distribution on a Delta Wing-body Space Shuttle Orbiter
Author: George E. Kaattari
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
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 : 778
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 778
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 964
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 : 964
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.
Hypersonic Lifting Body Windward Surface Flow-field Analysis for High Angles of Incidence
Author: John C. Adams (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 240
Book Description
Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 240
Book Description
Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.
Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. Kaattari
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Comparison of Hinge Moments for a Simple Delta Wing and a Delta-wing Orbiter Concept at Mach 6
Author: George C. Ashby
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Elevon hinge moments were determined from measured surface pressures on a typical delta-wing shuttle orbiter model at selective deflection angles for comparison with the extensive experimental and analytical hinge-moment data previously reported for a simple 75 [degrees] delta wing with a trailing-edge control. The angles of attack were from 0 [degrees] to 55 [degrees] at elevondeflection angles of -45.5 [degrees], O [degrees], and 20°. The results show that the elevon hinge moments on the shuttle orbiter are essentially the same as those measured earlier for the more basic model. Also included is an appendix describing a cubic spline function technique used to determine the hinge moments from elevon surface-pressure measurements.
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Elevon hinge moments were determined from measured surface pressures on a typical delta-wing shuttle orbiter model at selective deflection angles for comparison with the extensive experimental and analytical hinge-moment data previously reported for a simple 75 [degrees] delta wing with a trailing-edge control. The angles of attack were from 0 [degrees] to 55 [degrees] at elevondeflection angles of -45.5 [degrees], O [degrees], and 20°. The results show that the elevon hinge moments on the shuttle orbiter are essentially the same as those measured earlier for the more basic model. Also included is an appendix describing a cubic spline function technique used to determine the hinge moments from elevon surface-pressure measurements.
Pitot-pressure Distributions of the Flow Field of a Delta-wing Orbiter
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 172
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 172
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Book Description
Chemical Nonequilibrium Effects on the Inviscid Flow in the Windward Plane of Symmetry of Two Simplified Shuttle Configurations
Author: John A. Lordi
Publisher:
ISBN:
Category : Nonequilibrium thermodynamics
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Nonequilibrium thermodynamics
Languages : en
Pages : 52
Book Description