Investigation With An Interferometer Of The Turbulent Mixing Of A Free Supersonic Jet

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Investigation With An Interferometer Of The Turbulent Mixing Of A Free Supersonic Jet

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Author : Paul B. Gooderum
language : en
Publisher:
Release Date : 1949

Investigation With An Interferometer Of The Turbulent Mixing Of A Free Supersonic Jet written by Paul B. Gooderum and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.

The free turbulent mixing of a supersonic jet was investigated with an interferometer, of which a description is given. Density and velocity distributions through the mixing zone were obtained. The velocity distribution was found to be similar to those for imcompressible jets over only the subsonic portion of the mixing pattern.

Free Turbulent Mixing

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Author : Philip Thomas Harsha
language : en
Publisher:
Release Date : 1971

Free Turbulent Mixing written by Philip Thomas Harsha and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Turbulence categories.

Technical Note National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956

Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1975

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.

An Integral Analysis Of Heat Transfer Downstream Of A Rearward Facing Step With Small Coolant Injection

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Author : Keiichi Karashima
language : en
Publisher:
Release Date : 1970

An Integral Analysis Of Heat Transfer Downstream Of A Rearward Facing Step With Small Coolant Injection written by Keiichi Karashima and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aerodynamic heating categories.

Applied Mechanics Reviews

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Author :
language : en
Publisher:
Release Date : 1949

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Mechanics, Applied categories.

Annual Report National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957

Annual Report National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

List Of Technical Notes 1947 1953

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954

List Of Technical Notes 1947 1953 written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.

Measurements Of Section Characteristics Of A 45 Degree Swept Wing Spanning A Rectangular Low Speed Wind Tunnel As Affected By The Tunnel Walls

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Author : Robert E. Dannenberg
language : en
Publisher:
Release Date : 1950

Measurements Of Section Characteristics Of A 45 Degree Swept Wing Spanning A Rectangular Low Speed Wind Tunnel As Affected By The Tunnel Walls written by Robert E. Dannenberg and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamic load categories.

Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.

Analysis Of Wind Tunnel Tests To A Mach Number Of 0 90 Of A Four Engine Propeller Driving Airplane Configuration Having A Wing With 40 Degrees Sweepback And An Aspect Ratio Of 10

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Author : George G. Edwards
language : en
Publisher:
Release Date : 1956

Analysis Of Wind Tunnel Tests To A Mach Number Of 0 90 Of A Four Engine Propeller Driving Airplane Configuration Having A Wing With 40 Degrees Sweepback And An Aspect Ratio Of 10 written by George G. Edwards and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics categories.

An investigation has been conducted at speeds up to a Mach number of 0.90 to determine the effects of operating propellers on the longitudinal characteristics of a four-engine tractor airplane configuration having a 40 degrees swept wing with an aspect ratio of 10. Results of wind-tunnel tests of a model representing such an airplane configuration (see NACA TN 3789) show that these effects are of most concern in the low-speed high-thrust flight regime. In the present report the low-speed data are analyzed to determine the source of the various effects and to indicate how the adverse effects can be reduced, and the high-speed data are discussed primarily from the standpoint of Mach number effects. The analysis of the low-speed data indicates that the large variations of longitudinal stabil.itywith angle of attack resulted primarily from passage of the tail into and out of the slipstream. The slipstream also created large lift increments on the wing, particularly with flaps deflected, which resulted in increases in stability (with increasing thrust coefficient) from the outboard propeller and decreases in stability from the inboard propeller. It was concluded that the longitudinal stabiltty characteristics of the model couldbe improved by moving the nacelles outward, increasing the tail height, and reducing the tail span.