Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
Author: Byron M. Jaquet
Publisher:
Published: 1961
Total Pages: 22
ISBN-13:
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Author: Byron M. Jaquet
Publisher:
Published: 1961
Total Pages: 22
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DOWNLOAD EBOOKAuthor: Ross B. Robinson
Publisher:
Published: 1961
Total Pages: 42
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DOWNLOAD EBOOKAuthor: James F. Campbell
Publisher:
Published: 1967
Total Pages: 44
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DOWNLOAD EBOOKAuthor: Lloyd S. Jernell
Publisher:
Published: 1961
Total Pages: 32
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DOWNLOAD EBOOKAuthor: Thomas C. Kelly
Publisher:
Published: 1961
Total Pages: 68
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DOWNLOAD EBOOKAerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.
Author: Dennis E. Fuller
Publisher:
Published: 1963
Total Pages: 40
ISBN-13:
DOWNLOAD EBOOKAuthor: Ross B. Robinson
Publisher:
Published: 1960
Total Pages: 22
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DOWNLOAD EBOOKAuthor: Byron M. Jaquet
Publisher:
Published: 1963
Total Pages: 64
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DOWNLOAD EBOOKAuthor: Donn B. Kirk
Publisher:
Published: 1962
Total Pages: 32
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DOWNLOAD EBOOKAuthor: Thomas C. Kelly
Publisher:
Published: 1962
Total Pages: 80
ISBN-13:
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