Scientific and Technical Aerospace Reports PDF Download

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704

Book Description


Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration

Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration PDF Author: Arnold Polak
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 56

Book Description
Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data were obtained for a cone-cylinder-flare configuration. The experimental data were correlated with a theoretical prediction. (Author).

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388

Book Description


Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408

Book Description


An Experimental Investigation of Shock Wave -- Boundary Layer Interaction Dynamics

An Experimental Investigation of Shock Wave -- Boundary Layer Interaction Dynamics PDF Author: Gerald W. Braun
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 254

Book Description
Wind tunnel tests were performed which simulated the flow pulsations which are sometimes produced in engine inlets by shock-boundary layer interaction. Shock Mach numbers from 1.2 to 1.4 were used and the boundary layer was influenced by air bleeding in or sucking off. The flow was observed by shodowgraph and static and total pressures were measured by means of low frequency and high frequency response instruments. Static wall pressures, boundary layer pressure profiles, and total pressure distributions across several tunnel cross sections were plotted. The data were analyzed with respect to their rms value and power spectral density. A literature survey and an analytical investigation of the pulsations in a diffuser with nonviscous flow are included. (Author).

AGARD Conference Proceedings

AGARD Conference Proceedings PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 552

Book Description


Developments in Mechanics

Developments in Mechanics PDF Author:
Publisher:
ISBN:
Category : Mechanics
Languages : en
Pages : 1684

Book Description
Vol. for 1961 includes the proceedings of the 7th Midwestern Conference on Fluid Mechanics and the proceedings of the 5th Midwestern Conference on Solid Mechanics, both previously published seperately.

Japanese Science and Technology

Japanese Science and Technology PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 724

Book Description


Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 548

Book Description


Dissertation Abstracts

Dissertation Abstracts PDF Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 1018

Book Description