Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86
Title | Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86 PDF eBook |
Author | Dennis E. Fuller |
Publisher | |
Pages | 38 |
Release | 1963 |
Genre | Aerodynamics |
ISBN |
Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86
Title | Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86 PDF eBook |
Author | Dennis E. Fuller |
Publisher | |
Pages | 0 |
Release | 1963 |
Genre | Aerodynamics |
ISBN |
Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers
Title | Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers PDF eBook |
Author | Linda S. Bangert |
Publisher | |
Pages | 272 |
Release | 1992 |
Genre | Drag (Aerodynamics) |
ISBN |
The Effect of Afterbody Geometry on the Aerodynamic Characteristics of Rectangular Afterbodies at Transonic Mach Numbers
Title | The Effect of Afterbody Geometry on the Aerodynamic Characteristics of Rectangular Afterbodies at Transonic Mach Numbers PDF eBook |
Author | Linda S. Bangert |
Publisher | |
Pages | 224 |
Release | 1991 |
Genre | |
ISBN |
Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies
Title | Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies PDF eBook |
Author | Louis S. Stiver |
Publisher | |
Pages | 108 |
Release | 1971 |
Genre | Aerodynamic load |
ISBN |
Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers
Title | Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers PDF eBook |
Author | National Aeronautics and Space Administration (NASA) |
Publisher | Createspace Independent Publishing Platform |
Pages | 272 |
Release | 2018-07-24 |
Genre | |
ISBN | 9781723563997 |
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmetic fuselage model that simulates a twin-engine fighter. The effects of aft-end closure distribution (top/bottom) nozzle-flap boattail angle versus nozzle-sidewall boattail angle) and afterbody and nozzle corner treatment (sharp or radius) were investigated. Four different closure distributions with three different corner radii were tested. Tests were conducted over a range of Mach numbers from 0.40 to 1.25 and over a range of angles of attack from -3 to 9 degrees. Solid plume simulators were used to simulate the jet exhaust. For a given closure distribution in the range of Mach numbers tested, the sharp-corner nozzles generally had the highest drag, and the 2-in. corner-radius nozzles generally had the lowest drag. The effect of closure distribution on afterbody drag was highly dependent on configuration and flight condition. Bangert, Linda S. and Carson, George T., Jr. Langley Research Center NASA-TP-3236, L-17034, NAS 1.60:3236 RTOP 505-62-30-01...
The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01
Title | The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01 PDF eBook |
Author | John P. Gapcynski |
Publisher | |
Pages | 44 |
Release | 1960 |
Genre | Aerodynamic load |
ISBN |