Author: George E. KaattariPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
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
Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. KaattariEstimation of Shock Layer Thickness and Pressure Distribution on a Delta Wing-body Space Shuttle Orbiter
Author: George E. KaattariNASA Technical Note
Author: Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1508
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
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.
Monthly Catalog of United States Government Publications
Author: 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 DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Book Description
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.
Author: