Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. Kaattari
Publisher:
Published: 1971
Total Pages: 778
ISBN-13:
DOWNLOAD EBOOKPosts
Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. Kaattari
Publisher:
Published: 1971
Total Pages: 19
ISBN-13:
DOWNLOAD EBOOKEstimation of Shock Layer Thickness and Pressure Distribution on a Delta Wing-body Space Shuttle Orbiter
Author: George E. Kaattari
Publisher:
Published: 1971
Total Pages: 48
ISBN-13:
DOWNLOAD EBOOKPrediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations
Author: George E. Kaattari
Publisher:
Published: 1971
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKMonthly Catalogue, United States Public Documents
Author:
Publisher:
Published: 1971
Total Pages: 1508
ISBN-13:
DOWNLOAD EBOOKScientific and Technical Aerospace Reports
Author:
Publisher:
Published: 1982
Total Pages: 1282
ISBN-13:
DOWNLOAD EBOOKLists 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:
Published:
Total Pages: 1388
ISBN-13:
DOWNLOAD EBOOKMonthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
Published: 1976
Total Pages: 1408
ISBN-13:
DOWNLOAD EBOOKHypersonic Lifting Body Windward Surface Flow-field Analysis for High Angles of Incidence
Author: John C. Adams (Jr.)
Publisher:
Published: 1973
Total Pages: 240
ISBN-13:
DOWNLOAD EBOOKFormulation 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.
