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Estimation Of Attainable Leading Edge Thrust For Wings At Subsonic And Supersonic Speeds
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Book Synopsis Estimation of Attainable Leading-edge Thrust for Wings at Subsonic and Supersonic Speeds by : Harry W. Carlson
Download or read book Estimation of Attainable Leading-edge Thrust for Wings at Subsonic and Supersonic Speeds written by Harry W. Carlson and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Estimation of Attainable Leading-edge Thrust for Wings at Subsonicaand Supersonic Speeds by : Harry W. Carlson
Download or read book Estimation of Attainable Leading-edge Thrust for Wings at Subsonicaand Supersonic Speeds written by Harry W. Carlson and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Estimation of Leading-edge Thrust for Supersonic Wings of Arbitrary Planform by : Harry W. Carlson
Download or read book Estimation of Leading-edge Thrust for Supersonic Wings of Arbitrary Planform written by Harry W. Carlson and published by . This book was released on 1978 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Numerical Methods and a Computer Program for Subsonic and Supersonic Aerodynamic Design and Analysis of Wings with Attainable Thrust Considerations by :
Download or read book Numerical Methods and a Computer Program for Subsonic and Supersonic Aerodynamic Design and Analysis of Wings with Attainable Thrust Considerations written by and published by . This book was released on 1984 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Study of Supersonic Wings Employing the Attainable Leading-edge Thrust Concept by : Wilbur D. Middleton
Download or read book Study of Supersonic Wings Employing the Attainable Leading-edge Thrust Concept written by Wilbur D. Middleton and published by . This book was released on 1982 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Computer Program for Wing Subsonic Aerodynamic Performance Estimates Including Attainable Thrust and Vortex Lift Effects by : Harry W. Carlson
Download or read book A Computer Program for Wing Subsonic Aerodynamic Performance Estimates Including Attainable Thrust and Vortex Lift Effects written by Harry W. Carlson and published by . This book was released on 1982 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Improved Method for Prediction of Attainable Wing Leading-Edge Thrust by : Harry W. Carlson
Download or read book Improved Method for Prediction of Attainable Wing Leading-Edge Thrust written by Harry W. Carlson and published by . This book was released on 1996 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Estimation of Leading-edge Thrust for Supersonic Wings of Arbitrary Plabform by : Harry W. Carlson
Download or read book Estimation of Leading-edge Thrust for Supersonic Wings of Arbitrary Plabform written by Harry W. Carlson and published by . This book was released on 1978 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Wings with Significant Leading-edge Thrust at Cruise by : A. Warner Robins
Download or read book Supersonic Wings with Significant Leading-edge Thrust at Cruise written by A. Warner Robins and published by . This book was released on 1980 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Survey and Analysis of Research on Supersonic Drag-due-to-lift Minimization with Recommendations for Wing Design by : Harry W. Carlson
Download or read book Survey and Analysis of Research on Supersonic Drag-due-to-lift Minimization with Recommendations for Wing Design written by Harry W. Carlson and published by . This book was released on 1992 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Estimation of Wing Nonlinear Aerodynamic Characteristics at Supersonic Speeds by :
Download or read book Estimation of Wing Nonlinear Aerodynamic Characteristics at Supersonic Speeds written by and published by . This book was released on 1980 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms by : Maxwell Alfred Heaslet
Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Maxwell Alfred Heaslet and published by . This book was released on 1948 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Book Synopsis Theoretical Loading at Supersonic Speeds of Flat Swept-back Wings with Interacting Trailing and Leading Edges by : Doris Cohen
Download or read book Theoretical Loading at Supersonic Speeds of Flat Swept-back Wings with Interacting Trailing and Leading Edges written by Doris Cohen and published by . This book was released on 1949 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: By the method of superposition of conical flows, the load distribution is calculated for regions of a long swept-back wing behind the points at which the Mach lines from the trailing-edge apex intersect the leading edge. It is found that a good approximation on the load can be obtained by the application of a fairly simple correction factor to the two-dimensional subsonic distribution. The similarity of two-dimensional flow is used to derive expressions for the loss of lift behind the Mach lines from the tips of the wing.
Book Synopsis Estimation of Wing Nonlinear Aerodynamic Characteristics at Supersonic Speeds by : Harry W. Carlson
Download or read book Estimation of Wing Nonlinear Aerodynamic Characteristics at Supersonic Speeds written by Harry W. Carlson and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1992 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Derivatives of Triangular Wings at Supersonic Speeds by : Herbert S. Ribner
Download or read book Stability Derivatives of Triangular Wings at Supersonic Speeds written by Herbert S. Ribner and published by . This book was released on 1948 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds, given in NACA TN No. l423, is extended to apply to triangular wings having large vertex angles and traveling at supersonic speeds. The lift, rolling moment due to siderlip, and damping in roll and pitch for this more general case have been treated elsewhere on the basis of the theory of small disturbances.
