Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between Plus Or Minus 6.5 Degrees PDF Download
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Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
Author: T. Bradley Curry
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
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Author: Earl D. Knechtel
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 36
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Book Description
An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Author: Reginald R. Lundstrom
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 48
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Book Description
Two rocket models having cruciform, aspect-ratio-5, unwswept tails and a fineness-ratio-20 fuselage were flight tested over a Mach number range of approximately 1.7 to 2.4. One of the models had cruciform, aspect-ratio-3.4 forward surfaces in line with the tails. The models were given step disturbances by pulse rockets at intervals throughout the Mach number range and stability derivatives were obtained from the measured responses. The roll rates of the models varied from 10 radians per second to 5 radians per second.
Author: C. Donald Babb
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 82
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Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Author: Edward F. Ulmann
Publisher:
ISBN:
Category : Ballistic missiles
Languages : en
Pages : 34
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Book Description
Tests were conducted at Mach number 4.05 to determine the aerodynamic characteristics of several missile models having turbulent boundary layers and to compare these results with available method of predicting the aerodynamic characteristics. (The condition of the boundary layer was determined by the china-clay-lacquer boundary-layer-visualization technique.) Normal force and pitching moment were measured through an angle-of-attack range of 0 to between 4 and 8 degrees, depending upon balance limitations, and at roll angles of 0 and 45 degrees; drag was measured only at 0 degrees angle of attack.
Author: Robert F. Peck
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26
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Book Description
A rocket-propelled model of an airplane configuration having an arrow wing with 55 degree leading-edge sweep and a flat-sided fuselage mounting swept horizontal and vertical tails has been tested through use of the pulse-control technique at Mach numbers between 1.0 and 2.3. Results are presented from an investigation of longitudinal trim, lift, stability, drag, lateral force, thrust, and jet effects.
Author: Ross B. Robinson
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 38
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