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Effect Of Fin Arrangements On Aerodynamic Characteristics Of A Thick 74 Deg Delta Manned Lifting Entry Vehicle At Low Subsonic Speeds
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Book Synopsis Effect of Fin Arrangements on Aerodynamic Characteristics of a Thick 74 Deg Delta Manned Lifting Entry Vehicle at Low-subsonic Speeds by :
Download or read book Effect of Fin Arrangements on Aerodynamic Characteristics of a Thick 74 Deg Delta Manned Lifting Entry Vehicle at Low-subsonic Speeds written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Models of Two Thick 74 Deg Delta Manned Lifting Entry Vehicles at Low-subsonic Speeds by :
Download or read book Aerodynamic Characteristics of Models of Two Thick 74 Deg Delta Manned Lifting Entry Vehicles at Low-subsonic Speeds written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Flight Characteristics of a Model of the HL-10 Manned Lifting Entry Vehicle by : George M. Ware
Download or read book Investigation of the Flight Characteristics of a Model of the HL-10 Manned Lifting Entry Vehicle written by George M. Ware and published by . This book was released on 1967 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made of the low-subsonic flight characteristics of a model of the HL-10 manned lifting entry vehicle. This model was tested with two different center fins and with the larger center fin in combination with fin tips.
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1989 with total page 468 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration by : George M. Ware
Download or read book Transonic Aerodynamic Characteristics of a Proposed Assured Crew Return Capability (ACRC) Lifting-body Configuration written by George M. Ware and published by . This book was released on 1989 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 by : Robert S. Osborne
Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Low Subsonic Speeds of a Highly Swept Delta Wing Utilizing Nose Deflection for Control by : Bernard Spencer
Download or read book Longitudinal Aerodynamic Characteristics at Low Subsonic Speeds of a Highly Swept Delta Wing Utilizing Nose Deflection for Control written by Bernard Spencer and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels by : Bernard Spencer
Download or read book An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels written by Bernard Spencer and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.
Book Synopsis Transonic Aerodynamic Characteristics of a Manned Lifting Entry Vehicle with and Without Tip Fins by :
Download or read book Transonic Aerodynamic Characteristics of a Manned Lifting Entry Vehicle with and Without Tip Fins written by and published by . This book was released on 1966 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Elevon Deflection and of Model Components on Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers of 0.20 to 1.20 by :
Download or read book Effect of Elevon Deflection and of Model Components on Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers of 0.20 to 1.20 written by and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Characteristics of a Manned Lifting Entry Vehicle with Various Fins at Mach Numbers from 1.50 to 2.86 by :
Download or read book Stability Characteristics of a Manned Lifting Entry Vehicle with Various Fins at Mach Numbers from 1.50 to 2.86 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Full-scale Wind-tunnel Investigation of the Aerodynamic Characteristics of the HL-10 Manned Lifting Entry Vehicle by :
Download or read book Full-scale Wind-tunnel Investigation of the Aerodynamic Characteristics of the HL-10 Manned Lifting Entry Vehicle written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS by : Bernard Spencer
Download or read book AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS written by Bernard Spencer and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° by : Bernard Spencer
Download or read book High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° written by Bernard Spencer and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Low Speed of a Reentry Configuration Having Rigid Retractable Conical Lifting Surfaces by : Paul G. Fournier
Download or read book Aerodynamic Characteristics at Low Speed of a Reentry Configuration Having Rigid Retractable Conical Lifting Surfaces written by Paul G. Fournier and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Aerodynamic Characteristics of a Model of HL-10 Flight Research Vehicle with Basic and Modified Tip Pins by :
Download or read book Subsonic Aerodynamic Characteristics of a Model of HL-10 Flight Research Vehicle with Basic and Modified Tip Pins written by and published by . This book was released on 1971 with total page 572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical and Experimental Longitudinal Aerodynamic Characteristics of an Aspect Ratio 0.25 Sharp-edge Delta Wing at Subsonic, Supersonic, and Hypersonic Speeds by : Charles H. Fox
Download or read book Theoretical and Experimental Longitudinal Aerodynamic Characteristics of an Aspect Ratio 0.25 Sharp-edge Delta Wing at Subsonic, Supersonic, and Hypersonic Speeds written by Charles H. Fox and published by . This book was released on 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The suction analogy concept of Polhamus for predicting vortex lift in conjunction with an appropriate potential-flow solution is called the present method. This method is applied herein to an aspect ratio of 0.25 sharp-edge delta wing from a Mach number of 0.143 to 10.4 in free air and at 0.074 in ground effect, and also to an aspect ratio of 0.35 triangular cross-sectional body at Mach number of 6.9. The models had subsonic leading edges at the test Mach numbers. Vortex-flow effects could be neither confirmed nor denied to exist at high speeds because of the lack of flow visualization above a Mach number of 0.143. The data, however, could be better predicted by including a vortex-flow effect, although not always to the extent predicted from the present method because of the presence of actual and hypothesized unmodeled flow situations.