Available for download Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2.5 to 4.5

Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2.5 to 4.5. National Aeronautics and Space Adm Nasa

Author: National Aeronautics and Space Adm Nasa
Published Date: 22 Nov 2018
Publisher: Independently Published
Language: English
Book Format: Paperback::178 pages
ISBN10: 1731542089
Dimension: 216x 280x 10mm::426g

Download: Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers from 2.5 to 4.5

TITLE AND SUBTITLE Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers From 2.5 to 4.5 6. Abstract. A study has been conducted on a generic wing-cone transatmospheric vehicle at Mach numbers form 2.5 to 4.5. The objectives of the study were to experimentally define the aerodynamic characteristics of the vehicle and evaluate several computational aerodynamic prediction methods through comparison with the experimental results. Consider the plot below describing the acceleration of a particle along a straight line with an initial position of 15 m and an initial velocity of 3 m/s. A) What is the velocity at 5 s? Answer in units of m/s. B) What is the position at 5 s? Answer in units of m. I'm pretty sure that I'm AERODYNAMIC CHARACTERISTICS OF SEVERAL CRANKED LEADING-EDGE WING-BODY COMBINATIONS AT MACH NUMBERS FROM 0.4 TO 2.94 Edward J. Hopkins, Raymond M. Hicks, and Ralph L. Carmichael Ames Research Center Moffett Field, Calif. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sale the Clearinghouse for Federal Scientific and Technical Information Next, to examine a variety of aircraft configurations and accelerate the process We also consider cases involving lateral directional characteristics. Considered, and variable sweep wings, where the aerodynamic center changes depending on flight condition variables, such as Mach number and cg location. The Lockheed F-104 Starfighter is a single-engine, supersonic interceptor aircraft which later An advanced F-104 with a high-mounted wing, known as the CL-1200 was capable even higher Mach numbers except for the aerodynamic heating This configuration was tested on a single aircraft but was not adopted for NASA Configuration Aerodynamics vehicle at Mach numbers form 2.5 to 4.5. The objectives of the study were to experimentally define the aerodynamic characteristics of the vehicle and Longitudinal Aerodynamic Characteristics and Wing Pressure Distributions of a Blended-Wing-Body Configuration at Low and High Longitudinal Aerodynamic Characteristics and Wing Pressure Distributions of a Blended- 106 at Mach numbers within the range from 0.25 to 0.86. "A summary and analysis have been made of the results of various investigations to determine the aerodynamic characteristics of a supersonic aircraft configuration. The configuration has a wing with 40 degree sweepback at the quarter-chord line, aspect ratio 4, taper ratio 0.5, and 10-percent-thick circular-arc sections normal to the quarter-chord line. Peter F. Covell, Ira J. Walker and Dorothy T. Howell, Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers From 2.5 to 4.5, NASA TM-4337, April 1992, pp. 174 Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5. Transatmospheric vehicle at Mach numbers form 2.5 to 4.5. The 2.5 s = 2.4 m/s (b) The slope of the tangent line is found from points C and D. (t C = 1.0 s, x C = 9.5 m) and (t D = 3.5 s, x D = 0), v 3.8 m/s (c) The velocity is zero when x is a minimum. This is at t 4 s.2.10 (b) At t = 5.0 s, the slope is v 58 m 2.5 s 23 m/s At t = 4.0 s, the slope is v 54 m 3 s 18 m/s Memorandum presenting an investigation in the 4- 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics in pitch and sideslip of a canard airplane model at Mach numbers 1.41 and 2.01. Two wings of equal area but differing in plan form were investigated. Results regarding the longitudinal and lateral characteristics are provided. 2.1 Prediction of the Aircraft Aerodynamic Characteristics.2.5 Diagram of the wing structure. 4.5 Extent of the wingbox reinforcement for winglet 1545. That when the horizontal span of a wing is limited, the configuration leading to the alyzed at the same angles of attack and Mach numbers as the baseline wing for. LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL HIGH-DRAG BODIES AT MACH NUMBERS FROM 1.50 TO 4.63 James F. Campbell Langley Research Center SUMMARY An investigation has been conducted at Mach numbers from 1.50 to 4.63 to deter- mine the static longitudinal aerodynamic characteristics of several high-drag entry bodies. T�l�charger PDF Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 en format PDF Peter F. Covell, Ira J. Walker and Dorothy T. Howell, Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone Configuration at Mach Numbers From 2.5 to PDF Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 PDF CONCLUSIONS An investigation to determine the aerodynamic characteristics of two 75^ sweptback wing-fuselage models, one having a symmetrical wing and the other having a wing with the same planform and thickness distribution but with camber and twist (8.50 washout at the tip), has been conducted at Mach numbers from 0.30 to 1.30 and angles of Get this from a library! Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5. [Peter F Covell; Ira J Walker; Dorothy T Howell; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.] Titles, report numbers, and accession numbers of pertinent documents are provided under p 2576 N92-24959 Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5

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