Author: Willis Gene Steward
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
An Experimental Investigation of Base Pressure in a Supersonic Air Stream with Secondary Air Flow Into the Wake
Author: Willis Gene Steward
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Master's Theses and Doctoral Dissertations in the Pure and Applied Sciences
Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 518
Book Description
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 518
Book Description
New Experiments on Impact-pressure Interpretation in Supersonic and Subsonic Rarefied Air Streams
Author: F. S. Sherman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 73
Book Description
Results are presented of an experimental investigation of impact-pressure intrepretation in supersonic and subsonic rarefied air streams at Mach numbers from 0.1 and 1.7 to 3.4 and in the Reynolds number range from 2 to 800. A study of the effects of impact-probe size on the accuracy of pressure measurements indicated that corrections for viscous effects are less than 1 percent for probes in supersonic flows at Reynolds numbers above 200, where the Reynolds number is based on the velocity, density, and viscosity of the free stream, the reference dimension being the outer diameter of the probe. Viscous-effect corrections are presented for interpretation of pressure measurements at lower Reynolds numbers.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 73
Book Description
Results are presented of an experimental investigation of impact-pressure intrepretation in supersonic and subsonic rarefied air streams at Mach numbers from 0.1 and 1.7 to 3.4 and in the Reynolds number range from 2 to 800. A study of the effects of impact-probe size on the accuracy of pressure measurements indicated that corrections for viscous effects are less than 1 percent for probes in supersonic flows at Reynolds numbers above 200, where the Reynolds number is based on the velocity, density, and viscosity of the free stream, the reference dimension being the outer diameter of the probe. Viscous-effect corrections are presented for interpretation of pressure measurements at lower Reynolds numbers.
Masters Theses and Doctoral Dissertations in the Pure and Applied Sciences ... Accepted by Colleges and Universities of the United States
Author:
Publisher:
ISBN:
Category : Chemistry
Languages : en
Pages : 528
Book Description
Publisher:
ISBN:
Category : Chemistry
Languages : en
Pages : 528
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
Book Description
Preliminary Investigation of Momentum Diffusion Between Two Supersonic Airstreams in the Presence of Shock Waves
Author: John P. Weidner
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 82
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
Book Description
Journal of Basic Engineering
Author:
Publisher:
ISBN:
Category : Electrical engineering
Languages : en
Pages : 648
Book Description
Publisher:
ISBN:
Category : Electrical engineering
Languages : en
Pages : 648
Book Description
Transactions of the American Society of Mechanical Engineers
Author: American Society of Mechanical Engineers
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 1436
Book Description
Vols. 2, 4-11, 62-68 include the Society's Membership list; v. 55-80 include the Journal of applied mechanics (also issued separately) as contributions from the Society's Applied Mechanics Division.
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 1436
Book Description
Vols. 2, 4-11, 62-68 include the Society's Membership list; v. 55-80 include the Journal of applied mechanics (also issued separately) as contributions from the Society's Applied Mechanics Division.