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
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).
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
An Experimental Investigation of a Highly Underexpanded Sonic Jet Ejecting from a Flat Plate Into a Subsonic Crossflow
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.
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
32nd AIAA Fluid Dynamics Conference and Exhibit
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Book Description
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 Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1466
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1466
Book Description
Aerodynamic Interference Induced by Reaction Controls
Author: F. W. Spaid
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Scientific and Technical Aerospace Reports
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.
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.