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Prediction Of Static Aerodynamic Characteristics For Space Shuttle Like And Other Bodies At Angles Of Attack From 0 Degrees To 180 Degrees
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Book Synopsis Prediction of Static Aerodynamic Characteristics for Space-shuttle-like and Other Bodies at Angles of Attack from 0 Degrees to 180 Degrees by : Leland H. Jorgensen
Download or read book Prediction of Static Aerodynamic Characteristics for Space-shuttle-like and Other Bodies at Angles of Attack from 0 Degrees to 180 Degrees written by Leland H. Jorgensen and published by . This book was released on 1973 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Static Aerodynamic Characteristics for Space-shuttle-like and Other Bodies at Angles of Attack from 0 [degrees] to 180 [degrees] by : Leland H. Jorgensen
Download or read book Prediction of Static Aerodynamic Characteristics for Space-shuttle-like and Other Bodies at Angles of Attack from 0 [degrees] to 180 [degrees] written by Leland H. Jorgensen and published by . This book was released on 1973 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0.6 to 3.0 and Angles of Attack from 0 to 180 Deg by : William B. Baker (Jr.)
Download or read book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0.6 to 3.0 and Angles of Attack from 0 to 180 Deg written by William B. Baker (Jr.) and published by . This book was released on 1976 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack by : Leland H. Jorgensen
Download or read book Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack written by Leland H. Jorgensen and published by . This book was released on 1977 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Report written by and published by . This book was released on 1977 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1976 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack by : Leland Howard Jorgensen
Download or read book Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack written by Leland Howard Jorgensen and published by . This book was released on 1977 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 ̊to 90 ̊ by : Leland Howard Jorgensen
Download or read book A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 ̊to 90 ̊ written by Leland Howard Jorgensen and published by . This book was released on 1973 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1975 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1976 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen
Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1976 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by : Leland Howard Jorgensen
Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 written by Leland Howard Jorgensen and published by . This book was released on 1974 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Design Aerodynamic Prediction Methodology for Missiles with Nose Bluntness by : Charles W. Ingram
Download or read book Preliminary Design Aerodynamic Prediction Methodology for Missiles with Nose Bluntness written by Charles W. Ingram and published by . This book was released on 1978 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt: A semi-empirical methodology is presented for predicting the axial and normal force coefficients and the center of pressure to include nose bluntness effects for missiles. This methodology includes the transonic and supersonic Mach number regime with angles of attack from 0 to 180 degrees. This methodology correlates well with wind tunnel test data. (Author).
Download or read book NASA Contractor Report written by and published by . This book was released on 1984 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Induced Side Forces on Bodies of Revolution at High Angle of Attack by : Wardlaw, Jr. (Andrew B.)
Download or read book Induced Side Forces on Bodies of Revolution at High Angle of Attack written by Wardlaw, Jr. (Andrew B.) and published by . This book was released on 1975 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linear regression techniques are used to establish a quantitative description of side forces on bodies at high incidence. A data base is assembled concerning the key side force characteristics of maximum observed side force, angle of occurrence, and minimum angle of attack at which a side force is observed. This information is examined to determine the important trends and a predictive model for side force based on the crossflow analogy is developed to suggest other important variables. A linear regression model for these quantities is developed to include only those variables which are statistically significant. Results indicate that peak side force coefficients are a function of Mach number and only weakly of Reynolds number. Nose fineness is the critical model dimension which suggests that peak side force is a product of the nose flow field. The angle at which peak side forces occur is found to be dependent on model length and Mach number, while the onset angle of attack is a function of model length only.
Download or read book AIAA 74-101 - AIAA 74-150 written by and published by . This book was released on 1974 with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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