An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate Into a Subsonic Free Stream PDF Download

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An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate Into a Subsonic Free Stream

An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate Into a Subsonic Free Stream PDF Author: Troy A. Street
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 468

Book Description
An experimental investigation of the surface static pressures on a flat plate due to a jet injecting transversely into a subsonic free stream was conducted. The free stream Mach numbers were 0.1, 0.2, 0.4, and 0.6 and the jet total pressure ranged from 0 to 1200 psig. The results are presented in tabular form with representative examples of the data shown graphically. (Author).

An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate Into a Subsonic Free Stream

An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate Into a Subsonic Free Stream PDF Author: Troy A. Street
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 468

Book Description
An experimental investigation of the surface static pressures on a flat plate due to a jet injecting transversely into a subsonic free stream was conducted. The free stream Mach numbers were 0.1, 0.2, 0.4, and 0.6 and the jet total pressure ranged from 0 to 1200 psig. The results are presented in tabular form with representative examples of the data shown graphically. (Author).

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 648

Book Description


An Experimental Investigation of a Highly Underexpanded Sonic Jet Ejecting from a Flat Plate Into a Subsonic Crossflow

An Experimental Investigation of a Highly Underexpanded Sonic Jet Ejecting from a Flat Plate Into a Subsonic Crossflow PDF Author: Craig S. Shaw
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 100

Book Description
The induced static pressures due to a highly underexpanded sonic jet ejecting normally from a flat plate into a subsonic crosswind have been investigated. These pressure data have been recorded on the flat plate for a range of nominal jet-to-free-stream dynamic-pressure ratios from 0 to 1000 at free-stream Mach numbers of 0.1, 0.2, 0.4, and 0.6. The static pressure data measured on the flat plate are presented and correlated based upon the Riemann shock geometry in the jet plume. This data correlation improves with increasing free-stream Mach number.

A Correlation Method to Predict the Surface Pressure Distribution on an Infinite Plate from which a Jet is Issuing

A Correlation Method to Predict the Surface Pressure Distribution on an Infinite Plate from which a Jet is Issuing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 128

Book Description


32nd AIAA Fluid Dynamics Conference and Exhibit

32nd AIAA Fluid Dynamics Conference and Exhibit PDF Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 564

Book Description


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 : 1466

Book Description


Aerodynamic Interference Induced by Reaction Controls

Aerodynamic Interference Induced by Reaction Controls PDF Author: F. W. Spaid
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370

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.

Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 866

Book Description