Factors Affecting The Maximum Lift Drag Ratio At High Supersonic Speeds
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Author | : Charles H. McLellan |
Publisher | : |
Total Pages | : 22 |
Release | : 1956 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds Book in PDF, Epub and Kindle
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.
Author | : A. J. Eggers (Jr.) |
Publisher | : |
Total Pages | : 42 |
Release | : 1956 |
Genre | : Aerodynamics |
ISBN | : |
Download Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds Book in PDF, Epub and Kindle
Summary: The problem of designing an aircraft which will develop high lift-drag ratios in flight at high supersonic speeds is attacked using the elementary principle that the components of the aircraft should be individually and collectively arranged to impart the maximum downward and the minimum forward momentum to the surrounding air. This principle in conjunction with other practical considerations of hypersonic flight leads to the study of configurations for which the body is situated entirely below the wing; that is, flat-top wing-body combinations. Theory indicates that sensibly complete aircraft of this type can be designed to develop lift-drag ratios well in excess of 6.
Author | : Richard T. Whitcomb |
Publisher | : |
Total Pages | : 20 |
Release | : 1960 |
Genre | : Airplanes |
ISBN | : |
Download A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios Book in PDF, Epub and Kindle
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.
Author | : William J. Small |
Publisher | : |
Total Pages | : 66 |
Release | : 1966 |
Genre | : Hypersonic wind tunnels |
ISBN | : |
Download Effect of Geometric Modifications on the Maximum Lift-drag Ratios of Slender Wing-body Configurations at Hypersonic Speeds Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 66 |
Release | : 1994 |
Genre | : |
ISBN | : |
Download In-flight Lift-drag Characteristics for a Forward-swept Wing Aircraft and Comparisons with Contemporary Aircraft) Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 428 |
Release | : 1974 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : A.J. Jr Eggers |
Publisher | : |
Total Pages | : 36 |
Release | : 1956 |
Genre | : |
ISBN | : |
Download Aircraft Configurations Developed High Lift-drag Ratios at High Supersonic Speeds Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 28 |
Release | : 1966 |
Genre | : |
ISBN | : |
Download Current Methods for Prediction and Minimization of Lift Induced Drag at Supersonic Speeds Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 678 |
Release | : 1958 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download NACA Conference on High-Speed Aerodynamics Book in PDF, Epub and Kindle
Author | : Henry H. Arnaiz |
Publisher | : |
Total Pages | : 68 |
Release | : 1977 |
Genre | : B-70 bomber |
ISBN | : |
Download Flight-measured Lift and Drag Characteristics of a Large, Flexible, High Supersonic Cruise Airplane Book in PDF, Epub and Kindle