Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154
Book Description
Tables of Supersonic Flow Around Cones of Large Yaw
Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154
Book Description
Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 440
Book Description
Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 428
Book Description
Tables of Supersonic Flow Around Yawing Cones
Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 376
Book Description
Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodymanics, Supersonic
Languages : en
Pages : 432
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1216
Book Description
Approximations for the Thermodynamic and Transport Properties of High-temperature Air
Author: C. Frederick HansenPublisher:
ISBN:
Category : Air
Languages : en
Pages : 724
Book Description
The thermodynamic and transport prorerties of high-temperature air are found in closed form starting from approximate partition functions for the major components in air and neglecting all minor components. The compressibility, energy, entropy, the specific heats, the speed of sound, the coefficients of viscosity and of thermal conductivity, and the Prandtl numbers for air are tabulated from 500 degrees to 15,000 degrees K over a range of pressure from 0.0001 to 100 atmospheres. The enthalpy of air and the mol fractions of the major components of air can easily be found from the tabulated values for compressibility and energy. It is predicted that the Prandtl number for fully ionized air will become small compared to unity, the order of 0.01, and this implies that boundary layers in such flow will be very transparent to heat flux.
Technical Data Digest
Author: Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 770
Book Description
Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars
Author: Richard R. HeldenfelsPublisher:
ISBN:
Category : Box beams
Languages : en
Pages : 712
Book Description
A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.
Expected Number of Maxima and Minima of a Stationary Random Process with Non-Gaussian Frequency Distribution
Author: Franklin W. DiederichPublisher:
ISBN:
Category : Distribution (Probability theory)
Languages : en
Pages : 734
Book Description
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.