Effects Of Wing Position And Fuselage Size On The Low Speed Static And Rolling Stability Characteristics Of A Delta Wing Model PDF Download

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Effects of Wing Position and Fuselage Size on the Low-speed Static and Rolling Stability Characteristics of a Delta-wing Model

Effects of Wing Position and Fuselage Size on the Low-speed Static and Rolling Stability Characteristics of a Delta-wing Model
Author: Alex Goodman
Publisher:
Total Pages: 82
Release: 1954
Genre: Aeronautics
ISBN:

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An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.


Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 580
Release: 1956
Genre: Aeronautics
ISBN:

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Stresses Around Rectangular Cutouts in Torsion Boxes

Stresses Around Rectangular Cutouts in Torsion Boxes
Author: Paul Kuhn
Publisher:
Total Pages: 632
Release: 1953
Genre: Boxes
ISBN:

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A method is presented for calculating the stresses produced by rectangular cutouts of any size in torsion boxes. The problem is divided into a "box problem" and a "cover problem." The box problem is a special case of the general method of analyzing torsion boxes without cutouts. In the cover problem, simple shear-lag theory is used to obtain "key" stresses; the final distributions are obtained from these key stresses by means of simple rules or empirical distribution curves. Comparisons with the results from three series of tests in which the dimensions of the cutouts varied over a wide range are shown.


Expected Number of Maxima and Minima of a Stationary Random Process with Non-Gaussian Frequency Distribution

Expected Number of Maxima and Minima of a Stationary Random Process with Non-Gaussian Frequency Distribution
Author: Franklin W. Diederich
Publisher:
Total Pages: 734
Release: 1957
Genre: Distribution (Probability theory)
ISBN:

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A method is outlined for calculating the expected number of maxima or minima of a random process with non-Gaussian frequency distribution from the statistical moments of the process and its first two derivatives. This method is based on an estimate of the joint frequency function of the process and its first two derivatives given by mesm of a generalized form of Edgeworth's series; the procedure thus consists essentially in applying a correction to the results for a Gaussian process. The functions required in this procedure are calculated for the first two correction terms; therefore, the effects of skewness and kurtosis can be calculated, provided the required moments are known. Expressions are given for these moments in terms of multiple correlation functions and multi-spectra, and the relations between these functions for a random output of a linear system and those for the random input are indicated.


Technical Note

Technical Note
Author:
Publisher:
Total Pages: 468
Release: 1956
Genre: Aeronautics
ISBN:

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NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 484
Release: 1969
Genre:
ISBN:

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