Effects Of A Sting Support On The Supersonic Force And Moment Characteristics Of An Apollo Model At Angles From 30 Deg To 185 Deg
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Effects Of A Sting Support On The Supersonic Force And Moment Characteristics Of An Apollo Model At Angles From 30 Deg To 185 Deg
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Author :
language : en
Publisher:
Release Date : 1965
Effects Of A Sting Support On The Supersonic Force And Moment Characteristics Of An Apollo Model At Angles From 30 Deg To 185 Deg written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aeronautics categories.
Support Interference Of Wind Tunnel Models
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Author : Marie H. Tuttle
language : en
Publisher:
Release Date : 1981
Support Interference Of Wind Tunnel Models written by Marie H. Tuttle and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Aeronautics categories.
Popular Mechanics
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Author :
language : en
Publisher:
Release Date : 2000-01
Popular Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-01 with categories.
Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.
Effects Of Sting Support Interference On The Base Pressures Of A Model Having A Blunt Nosed Cylinder Body And A Conical Flare At Mach Numbers Of 0 65 To 2 20
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Author :
language : en
Publisher:
Release Date : 1960
Effects Of Sting Support Interference On The Base Pressures Of A Model Having A Blunt Nosed Cylinder Body And A Conical Flare At Mach Numbers Of 0 65 To 2 20 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
The Influence Of Sting And Strut Supports On The Aerodynamic Loads On An Ogive Cylinder At High Angles Of Attack At Transonic Speeds
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Author :
language : en
Publisher:
Release Date : 1980
The Influence Of Sting And Strut Supports On The Aerodynamic Loads On An Ogive Cylinder At High Angles Of Attack At Transonic Speeds written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with categories.
The influence of the model support system on an ogive cylinder at high angles of attack has been determined in transonic tests. Stings of varying diameter and struts in various orientations were studied. The stings did not alter the development of large side loads resulting from asymmetric vortex separation and had only moderate progressive effects on in-plane forces and moments. Struts supporting the model through its leeward meridian seriously altered normal and side forces and sharply reduced base drag at several combinations of Mach number and angle of attack. A strut supporting the model at its windward meridian (near the base) yielded results like those for the stings. (Author).
Spiked Blunt Bodies In Supersonic Flow
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Author : Hyman Harvey Album
language : en
Publisher:
Release Date : 1961
Spiked Blunt Bodies In Supersonic Flow written by Hyman Harvey Album and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic categories.
The force and moment characteristics of spiked bodies with hemispherical, hemispherical-flat, and flat noses were determined in a supersonic wind tunnel at angles of attack from zero to 10 degrees. The afterbodies were right circular cylinders. A fineness ratio of 3 was maintained for all of the basic bodies. The spikes were of five different configurations and ranged in length from 0.75 to 2.0 body diameters. Freestream conditions included Mach numbers from 2.0 to 3.0 and Reynolds numbers from 300,000 to 900,000 (based on body diameter). It was found that the spikes greatly reduced the zero-angle drag, made the drag extremely sensitive to angle of attack variations, substantially increased the lift, and also increased the normal force. The body nose shape proved to be a critical factor in determining the magnitude of these characteristics and whether or not the spikes would have a stabilizing effect on the body pitching moment characteristics. (Author).
Supersonic Aerodynamic Characteristics Of A Saturn Ib Launch Vehicle Model With Third Stage Modifications
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Author : Roger H. Fournier
language : en
Publisher:
Release Date : 1966
Supersonic Aerodynamic Characteristics Of A Saturn Ib Launch Vehicle Model With Third Stage Modifications written by Roger H. Fournier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
Subsonic Sting Interference On The Aerodynamic Characteristics Of A Family Of Slanted Base Ogive Cylinders
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Author : Colin P. Britcher
language : en
Publisher:
Release Date : 1990
Subsonic Sting Interference On The Aerodynamic Characteristics Of A Family Of Slanted Base Ogive Cylinders written by Colin P. Britcher and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aerodynamics categories.
Supersonic Aerodynamic Characteristics Of Some Reentry Concepts For Angles Of Attack To 90 Deg
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Author :
language : en
Publisher:
Release Date : 1985
Supersonic Aerodynamic Characteristics Of Some Reentry Concepts For Angles Of Attack To 90 Deg written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with categories.