Heat Transfer Distribution On 700 Swept Slab Delta Wings At A Mach Number Of 9 86 And Angles Of Attack Up To 900
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Heat Transfer Distribution On 700 Swept Slab Delta Wings At A Mach Number Of 9 86 And Angles Of Attack Up To 900
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Author : Philip E. Everhart
language : en
Publisher:
Release Date : 1964
Heat Transfer Distribution On 700 Swept Slab Delta Wings At A Mach Number Of 9 86 And Angles Of Attack Up To 900 written by Philip E. Everhart and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamics, Hypersonic categories.
Heat-transfer distributions were obtained on 700 swept slab delta wings with sharp and blunt noses and cylindrical leading edges. The free-stream Reynolds number based on model thickness was 9 x 10(4). Lees' theory for the heat-transfer distribution is shown to be in good agreement with the data obtained on the nose and leading edge. The point of peak heating on the leading edge is in close agreement with the Newtonian stagnation point at all angles of attack. At angles of attack from 40° to 60° cross-flow theory was in excellent agreement with experimental center-line data; however, at other model attitudes the theory differed significantly from experiment. Nose blunting resulted in reduced heating rates over the aft center-line section of the wing at angles of attack less than about 40°.
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.
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.
Heat Transfer Measurements At A Mach Number Of 4 95 On Two 60 Degree Sweot Delta Wings With Blunt Leading Edges And Dihedral Angles Of 0 Degrees And 46 Degrees
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Author : P. Calvin Stainback
language : en
Publisher:
Release Date : 1961
Heat Transfer Measurements At A Mach Number Of 4 95 On Two 60 Degree Sweot Delta Wings With Blunt Leading Edges And Dihedral Angles Of 0 Degrees And 46 Degrees written by P. Calvin Stainback and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Fluid mechanics categories.
Pressures And Heat Transfer On A 75 Swept Delta Wing With Trailing Edge Flap At Mach 6 And Angles Of Attack To 90
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Author : J. Wayne Keyes
language : en
Publisher:
Release Date : 1969
Pressures And Heat Transfer On A 75 Swept Delta Wing With Trailing Edge Flap At Mach 6 And Angles Of Attack To 90 written by J. Wayne Keyes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamic heating categories.
Pressure and heat transfer on swept delta wing with trailing-edge flap.
Heat Transfer And Pressure Measurements On Delta Wings At Mach Numbers Of 3 51 And 4 65 And Angles Of Attack From 45 To 45
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Author : Robert L. Stallings
language : en
Publisher:
Release Date : 1964
Heat Transfer And Pressure Measurements On Delta Wings At Mach Numbers Of 3 51 And 4 65 And Angles Of Attack From 45 To 45 written by Robert L. Stallings and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Airplanes categories.
Heat Transfer And Pressure Distributions On 60 And 70 Swept Delta Wings Having Turbulent Boundary Layers
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Author : William M. Murray (Jr.)
language : en
Publisher:
Release Date : 1966
Heat Transfer And Pressure Distributions On 60 And 70 Swept Delta Wings Having Turbulent Boundary Layers written by William M. Murray (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Airplanes categories.
Heat Transfer To A Delta Wing Half Cone Combination At Mach Numbers Of 7 And 10
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Author : James C. Dunavant
language : en
Publisher:
Release Date : 1964
Heat Transfer To A Delta Wing Half Cone Combination At Mach Numbers Of 7 And 10 written by James C. Dunavant and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamic heating categories.
Aeronautical Engineer S Data Book
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Author : Cliff Matthews
language : en
Publisher: Elsevier
Release Date : 2001-10-17
Aeronautical Engineer S Data Book written by Cliff Matthews and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001-10-17 with Technology & Engineering categories.
Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. Quick reference to essential data Most up to date information available
Fluid And Gasdynamics
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Author : G.H. Schnerr
language : en
Publisher: Springer Science & Business Media
Release Date : 2013-03-08
Fluid And Gasdynamics written by G.H. Schnerr and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-03-08 with Science categories.
This volume offers a wide range of theoretical, numerical and experimental research papers on fluid dynamics. The major fields of research - fundamentals of fluid mechanics as well as their applications - are treated: - stability phenomena: convective flow, thermal and hydrodynamic systems - transition, turbulence and separation: boundary-layer, turbulent combustion, rarefied gasdynamics, near wall and off wall flow fields, energy dissipation - transonic flow: homogeneous condensation, shock-waves, effects at Mach number unity - hypersonic flow: flow over spheres, aerothermodynamics, relaxation - fluid machinery: axial fans, compressor cascades, fluid couplings - computational fluid dynamics: passive shock control, zonal computation, cylinderflow, flow over wings - miscellaneous problems.