Experimental Investigation Of Supersonic Flow With Detached Shock Waves For Mach Numbers Between 18 And 29 PDF Download
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Author | : W. E. Moeckel |
Publisher | : |
Total Pages | : 56 |
Release | : 1950 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Experimental Investigation of Supersonic Flow with Detached Shock Waves for Mach Numbers Between 1.8 and 2.9 Book in PDF, ePub and Kindle
Results of an experimental investigation of the flow near the nose of plane and axially symmetric bodies in the presence of detached shock waves are compared with predictions of theory. The location of the detached shock wave was determined from schlieren photographs for a variety of nose shapes over a range of free-stream Mach numbers from 1.8 to 2.9. At a Mach number of 1.9, the form of the detached wave and the pressure distribution over the body were investigated for each nose shape. In addition, the relation between shock location and flow spillage was determined for several axially symmetric nose inlets.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 388 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
Author | : E. V. Laitone |
Publisher | : |
Total Pages | : 50 |
Release | : 1950 |
Genre | : Ultrasonic waves |
ISBN | : |
Download An Experimental Investigation of Transonic and Accelerated Supersonic Flow by the Hydraulic Analogy Book in PDF, ePub and Kindle
Author | : Arthur Earl Bryson |
Publisher | : |
Total Pages | : 106 |
Release | : 1951 |
Genre | : Aerodynamic load |
ISBN | : |
Download An Experimental Investigation of Transonic Flow Past Two-dimensional Wedge and Circular-arc Sections Using a Mach-Zehnder Interferometer Book in PDF, ePub and Kindle
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc sections at zero angle of attack. Pressure distributions and drag coefficients as functions of Mach number were obtained and the wedge data are compared with theory. It is shown that the local Mach number at any point on the surface of a finite three dimensional body or an unswept two-dimensional body, moving through an infinite fluid, has a stationary value at Mach number 1 and, in fact, remains nearly constant for a range of speeds below and above Mach number 1. On the basis of this concept and the experimental data, pressure distributions and drag coefficients for the wedge and circular-arc sections are presented throughout the entire transonic range of velocities.
Author | : |
Publisher | : |
Total Pages | : 750 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : |
Download Annual Report - National Advisory Committee for Aeronautics Book in PDF, ePub and Kindle
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 442 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Download Research Abstracts Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : |
Release | : 1982 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : Arthur Earl Bryson |
Publisher | : |
Total Pages | : 340 |
Release | : 1952 |
Genre | : Aeronautics |
ISBN | : |
Download Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle
Author | : E. R. G. Eckert |
Publisher | : |
Total Pages | : 330 |
Release | : 1955 |
Genre | : Aerodynamics |
ISBN | : |
Download Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method Book in PDF, ePub and Kindle