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The Leading Edge Effects On The Laminar Flat Plate Boundary Layer And The Aerodynamic Heating At Mach 104
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Book Synopsis The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 by : Howard W. Stone
Download or read book The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 written by Howard W. Stone and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 by : Howard W. Stone
Download or read book The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 written by Howard W. Stone and published by . This book was released on 1969 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 by : Marcus O. Creager
Download or read book Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 written by Marcus O. Creager and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 by : Earl A. Price
Download or read book Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 written by Earl A. Price and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 by : Thorval Tendeland
Download or read book The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 written by Thorval Tendeland and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Compressible Laminar Boundary Layer with Fluid Injection by : George M. Low
Download or read book The Compressible Laminar Boundary Layer with Fluid Injection written by George M. Low and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A solution of the equations of the compressible laminar boundary layer including the effects of transpiration cooling is presented. The analysis applies to the flow over an isothermal porous plate with a velocity of fluid injection proportional to the reciprocal of the square root of the distance from the leading edge.
Book Synopsis The Leading-edge Effects on a Laminar Flat-plane Boundary Layer at Mach 10.4 by : Howard W. Stone
Download or read book The Leading-edge Effects on a Laminar Flat-plane Boundary Layer at Mach 10.4 written by Howard W. Stone and published by . This book was released on 1968 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 by : Robert L. O'Neal
Download or read book Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 written by Robert L. O'Neal and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0 by : Paul F. Holloway
Download or read book An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0 written by Paul F. Holloway and published by . This book was released on 1965 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate by : Don W. Jillie
Download or read book Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate written by Don W. Jillie and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution by : Raul J. Conti
Download or read book Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul J. Conti and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles by : E. C. Lemmon
Download or read book The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles written by E. C. Lemmon and published by . This book was released on 1971 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Two-dimensional Multiple Sine-wave Protrusions on the Pressure and Heat-transfer Distributions for a Flat Plate at Mach 6 by : Aubrey M. Cary
Download or read book 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 published by . This book was released on 1968 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :956 pages Book Rating :4.:/5 (317 download)
Book Synopsis NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution by : Raul Jorge Conti
Download or read book Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul Jorge Conti and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 1346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Fin Leading-edge Shape on Aerodynamic Heating at Mach Number 2.0 at a Stagnation Temperature of about 2,600 Degrees R by : William M. Bland
Download or read book Some Effects of Fin Leading-edge Shape on Aerodynamic Heating at Mach Number 2.0 at a Stagnation Temperature of about 2,600 Degrees R written by William M. Bland and published by . This book was released on 1958 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three un-instrumented tapered magnesium fins with the leading edges swept back 17 degrees have been tested in an ethylene-heated high-temperature jet at the Langley Pilotless Aircraft Research Station at Wallops Island, Virginia. These tests were made to investigate some effects of leading-edge diameter and leading-edge shape on the aerodynamic heating by noting the time for melting to begin on the fins. Results of these tests, which were conducted at a Mach number of 2.0 for stagnation temperatures in the neighborhood of 2,600 degrees R, indicate that increasing the diameter of the cylindrical leading edge increased the time required for melting to start. This increase was greater, probably because of conduction effects, than that predicted by relating the time to melt inversely with the square root of leading-edge diameter. Also, the model with the flat-face leading edge lasted 1.39 times as long as the model with about the same size cylindrical leading edge.
