Damping In Roll Of Cruciform And Some Related Delta Wings At Supersonic Speeds PDF Download

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Damping in Roll of Cruciform and Some Related Delta Wings at Supersonic Speeds

Damping in Roll of Cruciform and Some Related Delta Wings at Supersonic Speeds
Author: Herbert S. Ribner
Publisher:
Total Pages: 50
Release: 1951
Genre: Aerodynamics, Supersonic
ISBN:

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The damping in roll of cruciform delta wings in supersonic flow has been evaluated by means of small-disturbance (linearized) wing theory; both subsonic and supersonic component stream velocities normal to the leading edges have been considered. In addition, some known two-dimensional results for rotating multibladed laminae have been applied to obtain the loading when the number of panels is changed from four to an arbitrary number, under the restriction of low aspect ratio; the damping in roll has been determined explicitly for three panels. Finally, the damping for an inifinite number of panels has been evaluated without restriction as to aspect ratio or Mach number.


Technical Note

Technical Note
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 818
Release: 1951
Genre: Aeronautics
ISBN:

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Vortex Interference on Slender Airplanes

Vortex Interference on Slender Airplanes
Author: Alvin H. Sacks
Publisher:
Total Pages: 702
Release: 1955
Genre: Airplanes
ISBN:

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It is found that the impulse of each shed vortex and its image vortex in a transformed circle plane enters into all the interference forces and moments on the airplane. A simple theorem is given for the interference forces in steady straight flight which are found to depend on this impulse evaluated only at the wing trailing edge and at the base of the configuration.


Methods for Obtaining Desired Helicopter Stability Characteristics and Procedures for Stability Predictions

Methods for Obtaining Desired Helicopter Stability Characteristics and Procedures for Stability Predictions
Author: F. B. Gustafson
Publisher:
Total Pages: 720
Release: 1957
Genre: Aeronautics
ISBN:

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Part 1 of this report presents a brief review of methods available to the helicopter designer for obtaining desired stability characteristics by modifications to the airframe design. The discussion is based on modifications made during the establishment of flying-qualities criteria and includes sample results of theoretical studies of additional methods. The conclusion is reached that it is now feasible to utilize combinations of methods whereby stability-parameter values are realized which in turn provide the desired stability characteristics. Part 2 reviews some of the methods of predicting rotor stability derivatives. The procedures by which these rotor derivatives are employed to estimate helicopter stability characteristics have been summarized.


Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 1200
Release: 1954
Genre: Aeronautics
ISBN:

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.