Author: Mitchel H. Bertram
Publisher:
Published: 1963
Total Pages: 136
ISBN-13:
DOWNLOAD EBOOK →Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.
Author: UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
Publisher:
Published:
Total Pages: 100
ISBN-13:
DOWNLOAD EBOOK →Author: John C. Adams (Jr.)
Publisher:
Published: 1973
Total Pages: 240
ISBN-13:
DOWNLOAD EBOOK →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: United States. National Aeronautics and Space Administration
Publisher:
Published: 1963
Total Pages: 930
ISBN-13:
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