Wind-tunnel-flight Correlation of Shock-induced Separated Flow

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.81/5 ( download)

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Book Synopsis Wind-tunnel-flight Correlation of Shock-induced Separated Flow by : Donald L. Loving

Download or read book Wind-tunnel-flight Correlation of Shock-induced Separated Flow written by Donald L. Loving and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Study of Effects of Reynolds Number and Boundary-layer Transition Location on Shock-induced Separation

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.35/5 ( download)

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Book Synopsis Preliminary Study of Effects of Reynolds Number and Boundary-layer Transition Location on Shock-induced Separation by : James A. Blackwell (Jr.)

Download or read book Preliminary Study of Effects of Reynolds Number and Boundary-layer Transition Location on Shock-induced Separation written by James A. Blackwell (Jr.) and published by . This book was released on 1969 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.21/5 ( download)

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Book Synopsis Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number by : J. F. Cahill

Download or read book Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number written by J. F. Cahill and published by . This book was released on 1979 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Effects of Trailing-edge Geometry on a NASA Supercritical Airfoil Section

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.67/5 ( download)

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Book Synopsis Wind-tunnel Investigation of Effects of Trailing-edge Geometry on a NASA Supercritical Airfoil Section by : Charles D. Harris

Download or read book Wind-tunnel Investigation of Effects of Trailing-edge Geometry on a NASA Supercritical Airfoil Section written by Charles D. Harris and published by . This book was released on 1971 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 920 pages
Book Rating : 4.3Z/5 ( download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 920 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Naval Research Reviews

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ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.38/5 ( download)

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Book Synopsis Naval Research Reviews by :

Download or read book Naval Research Reviews written by and published by . This book was released on 1974 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Integral Equation Method for Boundary Interference in a Perforated-wall Wind Tunnel at Transonic Speeds

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.98/5 ( download)

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Book Synopsis An Integral Equation Method for Boundary Interference in a Perforated-wall Wind Tunnel at Transonic Speeds by : E. M. Kraft

Download or read book An Integral Equation Method for Boundary Interference in a Perforated-wall Wind Tunnel at Transonic Speeds written by E. M. Kraft and published by . This book was released on 1976 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: The wind tunnel boundary interference at transonic speeds on a thin airfoil in a two-dimensional perforated-wall wind tunnel was determined. The interference was found by applying an integral equation method to the nonlinear transonic small disturbance equation including embedded supersonic regions with shock waves. The kernels of the ensuing integral equation were replaced by series approximations, and the integrals were evaluated in closed form. The iterative technique used to calculate the interference from the integral equation method is shown to converge rapidly, and the computing time for the integral equation method is typically an order of magnitude less than present numerical methods. As a special case, the integral equation method for a thin airfoil in free air was also examined. It was found that the introduction of a novel influence function yields, for the first time, a self-contained integral equation for a lifting airfoil. In addition, a systematic study of the classical assumption used to simplify the integral equation shows that the integral method can provide solutions in good agreement with results from the numerical methods.

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 558 pages
Book Rating : 4.15/5 ( download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1976 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government-wide Index to Federal Research & Development Reports

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ISBN 13 :
Total Pages : 1466 pages
Book Rating : 4.85/5 ( download)

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Book Synopsis Government-wide Index to Federal Research & Development Reports by :

Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1966 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research & Development Reports

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ISBN 13 :
Total Pages : 1014 pages
Book Rating : 4.14/5 ( download)

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Book Synopsis U.S. Government Research & Development Reports by :

Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1014 pages. Available in PDF, EPUB and Kindle. Book excerpt: