An Experimental Study Of The Pressure And Heat Transfer Distribution On A 70 Sweep Slab Delta Wing In Hypersonic Flow

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An Experimental Study Of The Pressure And Heat Transfer Distribution On A 70 Sweep Slab Delta Wing In Hypersonic Flow

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Author : Mitchel H. Bertram
language : en
Publisher:
Release Date : 1963

An Experimental Study Of The Pressure And Heat Transfer Distribution On A 70 Sweep Slab Delta Wing In Hypersonic Flow written by Mitchel H. Bertram and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Airplanes categories.

Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.

An Experimental Study Of The Pressure And Heat Transfer Distribution On A 70 Sweep Slab Delta Wing In Hypersonic Flow

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Author : Mitchel H. Bertram
language : en
Publisher:
Release Date : 1963

An Experimental Study Of The Pressure And Heat Transfer Distribution On A 70 Sweep Slab Delta Wing In Hypersonic Flow written by Mitchel H. Bertram and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics, Hypersonic categories.

Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.

Hypersonic Lifting Body Windward Surface Flow Field Analysis For High Angles Of Incidence

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Author : John C. Adams (Jr.)
language : en
Publisher:
Release Date : 1973

Hypersonic Lifting Body Windward Surface Flow Field Analysis For High Angles Of Incidence written by John C. Adams (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aerodynamics, Hypersonic categories.

Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1971

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 1971 with categories.

Pressure Distributions On Blunt Delta Wings At Angles Of Attack Up To 90 Degrees And Mach Number Of 6 85

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Author : Peter T. Bernot
language : en
Publisher:
Release Date : 1963

Pressure Distributions On Blunt Delta Wings At Angles Of Attack Up To 90 Degrees And Mach Number Of 6 85 written by Peter T. Bernot and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Mach number categories.

Nasa Technical Report

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1963

Nasa Technical Report written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1972

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aeronautics categories.

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.

Effect Of Two Dimensional Multiple Sine Wave Protrusions On The Pressure And Heat Transfer Distributions For A Flat Plate At Mach 6

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Author : Aubrey M. Cary
language : en
Publisher:
Release Date : 1968

Effect Of Two Dimensional Multiple Sine Wave Protrusions On The Pressure And Heat Transfer Distributions For A Flat Plate At Mach 6 written by Aubrey M. Cary and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aerodynamic heating categories.

Turbulent Boundary Layer Heat Transfer And Transition Measurements With Surface Cooling At Mach 6

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Author : Aubrey M. Cary
language : en
Publisher:
Release Date : 1970

Turbulent Boundary Layer Heat Transfer And Transition Measurements With Surface Cooling At Mach 6 written by Aubrey M. Cary and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Heat categories.

The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Theory And Applications

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Author : Chong-Wei Chu
language : en
Publisher:
Release Date : 1972

The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Theory And Applications written by Chong-Wei Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics, Supersonic categories.