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Low Speed Wind Tunnel Investigation Of High Lift Devices On A 65 Degree Swept Back Supersonic Wing Of 344 Aspect Ratio
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Book Synopsis Low Speed Wind Tunnel Investigation of High Lift Devices on a 65 Degree Swept-back Supersonic Wing of 3.44 Aspect Ratio by : Michael F. Marx
Download or read book Low Speed Wind Tunnel Investigation of High Lift Devices on a 65 Degree Swept-back Supersonic Wing of 3.44 Aspect Ratio written by Michael F. Marx and published by . This book was released on 1949 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Low-speed High-lift Aerodynamics of a One-fifth Scale Variable-sweep Supersonic Transport by : Anthony M. Cook
Download or read book Wind-tunnel Investigation of the Low-speed High-lift Aerodynamics of a One-fifth Scale Variable-sweep Supersonic Transport written by Anthony M. Cook and published by . This book was released on 1968 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Investigation of the Low-speed Aerodynamic Characteristics of a Supersonic Transport Model Having Variable-sweep Wings by : Anthony M. Cook
Download or read book Large-scale Wind-tunnel Investigation of the Low-speed Aerodynamic Characteristics of a Supersonic Transport Model Having Variable-sweep Wings written by Anthony M. Cook and published by . This book was released on 1965 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Studies Relating to Pitch-up on a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Wing by : Vernard E. Lockwood
Download or read book Low-speed Wind-tunnel Studies Relating to Pitch-up on a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Wing written by Vernard E. Lockwood and published by . This book was released on 1966 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Effects of Canard Planform and Wing High-lift Devices on the Longitudinal Aerodynamic Characteristics of a Supersonic Transport Configuration by :
Download or read book Low-speed Wind-tunnel Investigation of the Effects of Canard Planform and Wing High-lift Devices on the Longitudinal Aerodynamic Characteristics of a Supersonic Transport Configuration written by and published by . This book was released on 1963 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Effects of High-lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails by : William C. Sleeman
Download or read book Low-speed Effects of High-lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails written by William C. Sleeman and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings by : Willard G. Smith
Download or read book A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings written by Willard G. Smith and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind Tunnel Investigation of the Aerodynamic Characteristics of High-lift Devices on Supersonic Wings at Low Subsonic Speed by : Philip G. Blenkush
Download or read book A Wind Tunnel Investigation of the Aerodynamic Characteristics of High-lift Devices on Supersonic Wings at Low Subsonic Speed written by Philip G. Blenkush and published by . This book was released on 1949 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing - Effects of External Fuel Tanks and Rocket Packets on the Drag Characteristics by : Willard G. Smith
Download or read book Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing - Effects of External Fuel Tanks and Rocket Packets on the Drag Characteristics written by Willard G. Smith and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios by : Richard T. Whitcomb
Download or read book A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios written by Richard T. Whitcomb and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body combinations at moderate supersonic speeds with axial developments of cross-sectional area has been derived. The wave drag of a combination at a given supersonic speed is related to a number of developments of cross-sectional areas as intersected by Mach planes. On the basis of this concept and other design procedures, a structurally feasible, swept-wing--indented-body combination has been designed to have relatively high maximum lift-drag ratios over a range of transonic and moderate supersonic Mach numbers. The wing of the combination has been designed to have reduced drag associated with lift and, when used with an indented body, to have low zero-lift wave drag. Experimental results have been obtained for this configuration at Mach numbers from 0.80 to 2.01. Maximum lift-drag ratios of approximately 14 and 9 were measured at Mach numbers of 1.15 and 1.41, respectively.
Book Synopsis Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing - Stability and Control by : Willard G. Smith
Download or read book Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing - Stability and Control written by Willard G. Smith and published by . This book was released on 1953 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 by : Davis S. Miller
Download or read book Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 written by Davis S. Miller and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds by : Charles H. McLellan
Download or read book Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds written by Charles H. McLellan and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.
Book Synopsis Low-speed wind-tunnel investigation of a large-scale advanced arrow-wing supersonic transport configuration with engines mounted above wings for upper-surface blowing by : James P. Shivers
Download or read book Low-speed wind-tunnel investigation of a large-scale advanced arrow-wing supersonic transport configuration with engines mounted above wings for upper-surface blowing written by James P. Shivers and published by . This book was released on 1976 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High-speed Wind Tunnels by : Luigi Crocco
Download or read book High-speed Wind Tunnels written by Luigi Crocco and published by . This book was released on 1946 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt: The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.
Book Synopsis Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices by : W. Kreuger
Download or read book Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices written by W. Kreuger and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane by : James C. Daugherty
Download or read book Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane written by James C. Daugherty and published by . This book was released on 1961 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
