Download or read book Some Aerodynamic and Control Studies of Lifting Reentry Configurations at Angles of Attack Up to 90 at a Mach Number of 2 91 written by Frank L. Clark and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1 97 and Angles of Attack Up to 90 written by Gerald V. Foster and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Keywords Index to U S Government Technical Reports written by and published by . This book was released on 1962 with total page 1160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Keywords Index to U S Government Technical Reports permuted Title Index written by United States. Department of Commerce. Office of Technical Services and published by . This book was released on 1963 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Blunted Right Triangular Pyramidal Lifting Reentry Configuration for Angles of Attack Up to 110 written by John P. Mugler and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Longitudinal and Lateral Controls on Aerodynamic Characteristics of a Winged Reentry Configuration at a Mach Number of 1 97 and Angles of attack Up to Approximately 90 written by Gerald V. Foster and published by . This book was released on 1961 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Control surface Instabilities on Lifting body Reentry Vehicles at a Mach Number of 15 4 written by Robert Charles Goetz and published by . This book was released on 1971 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Aerodynamic Characteristics of a Right Triangular Pyramidal Lifting Reentry Configuration at Mach Numbers of 3 00 4 50 and 6 00 for Angles of Attack Up to 56 Deg written by and published by . This book was released on 1962 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2 86 and 6 02 and Angles of Attack Up to 95 Deg of a Lenticular shaped Reentry Vehicle written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Control Characteristics of a Flat bottom Lifting Reentry Configuration at Mach Numbers of 2 29 to 4 63 written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Aerodynamic Characteristics at Triangular Pyramidal Lifting Reentry Configuration for Angles of Attack Up to 110 Degrees written by JOHN P. JR. MUGLER and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static longitudinal aerodynamic characteristics of a blunted right triangular pyramidal lifting reentry configuration have been obtainedAT Mach numbers from 0.60 to 1.20 and angles of attack from 0 degrees to 110 degrees. The test Reynolds number, based on the mean geometric chord, varied during the tests from about 2.2 x 10 to the 6th power to 5.7 x 10 to the 6th power. The results indicate that the model was statically longitudinally stable near 0 degrees and 90 degrees angle of attack; however, the onset of pitch-up caused unstable or neutrally stable regions between angles of attack of about 25 degrees to 50 degrees. Maximum lift-drag ratios of about 2.4 were obtained at subsonic speeds and then diminished to about 1.6 at low supersonic speeds. Comparisons with data from other tests indicate that blunting the nose, leading edge, and ridge line had little effect on the maximum lift-drag ratio. (Author).
Download or read book Stability and Control Characteristics of a Low lift drag ratio Reentry Vehicle at Mach Numbers from 2 30 to 4 65 written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability and Control Characteristics of a Flat bottom Lifting Reentry Configuration at a Mach Number of 1 61 written by and published by . This book was released on 1964 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Studies of Stability and Control of Winged Reentry Configurations written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Stability and Control Characteristics of a Right Triangular Pyramid Lifting Reentry Configuration at a Mach Number of 10 03 written by and published by . This book was released on 1964 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Aerodynamic Characteristics of a Reentry Vehicle Configuration Having an Extendable Leading Edge at a Mach Number of 10 03 and Angles of Attack from 50 Deg to 90 Deg written by and published by . This book was released on 1963 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
