Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds

Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds
Author :
Publisher :
Total Pages : 36
Release :
ISBN-10 : UIUC:30112106773705
ISBN-13 :
Rating : 4/5 (05 Downloads)

Book Synopsis Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds by : K. R. Czarnecki

Download or read book Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds written by K. R. Czarnecki and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds Related Books

Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds
Language: en
Pages: 36
Authors: K. R. Czarnecki
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

Effects of Unit Reynolds Number, Nose Bluntness, and Roughness on Boundary Layer Transition
Language: en
Pages: 166
Authors: J. Leith Potter
Categories: Boundary layer
Type: BOOK - Published: 1960 - Publisher:

DOWNLOAD EBOOK

Condtions encountered in the high Mach number flow regime are show to profoundly affect the longitudinal extent of the boundary layer from beginning to end of t
Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate
Language: en
Pages: 36
Authors: Don W. Jillie
Categories: Fluid mechanics
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

Investigation of the Effects of Low Reynolds Number Operation on the Performance of a Single-Stage Turbine with a Downstream Stator
Language: en
Pages: 52
Authors: Robert E. Forrette
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

Effects of Reynolds Number and Flow Incidence on the Force Characteristics of a Family of Flat-front Cylinders
Language: en
Pages: 50
Authors: Vernard E. Lockwood
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1967 - Publisher:

DOWNLOAD EBOOK