Stability of Two Rocket-propelled Models Having Aspect-ratio-5 Unswept Tails on a Long Body for the Mach Number Range of 1.7 to 2.4 PDF Download

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Stability of Two Rocket-propelled Models Having Aspect-ratio-5 Unswept Tails on a Long Body for the Mach Number Range of 1.7 to 2.4

Stability of Two Rocket-propelled Models Having Aspect-ratio-5 Unswept Tails on a Long Body for the Mach Number Range of 1.7 to 2.4 PDF Author: Reginald R. Lundstrom
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 48

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.

Stability of Two Rocket-propelled Models Having Aspect-ratio-5 Unswept Tails on a Long Body for the Mach Number Range of 1.7 to 2.4

Stability of Two Rocket-propelled Models Having Aspect-ratio-5 Unswept Tails on a Long Body for the Mach Number Range of 1.7 to 2.4 PDF Author: Reginald R. Lundstrom
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 48

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.

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