Aerodynamics of a Model of the HL-10 Flight-test Vehicle at Mach 0.35 to 1.80
Author: Charles L. Ladson
Publisher:
Published: 1971
Total Pages: 140
ISBN-13:
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Author: Charles L. Ladson
Publisher:
Published: 1971
Total Pages: 140
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DOWNLOAD EBOOKAuthor: Robert W. Kempel
Publisher:
Published: 1974
Total Pages: 52
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DOWNLOAD EBOOKAuthor: George M. Ware
Publisher:
Published: 1967
Total Pages: 46
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DOWNLOAD EBOOKAn investigation has been made of the low-subsonic flight characteristics of a model of the HL-10 manned lifting entry vehicle. This model was tested with two different center fins and with the larger center fin in combination with fin tips.
Author: Robert W. Kempel
Publisher:
Published: 1994
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1971
Total Pages: 572
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DOWNLOAD EBOOKAuthor: Edwin J. Saltzman
Publisher:
Published: 2002
Total Pages: 162
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DOWNLOAD EBOOKAuthor: Larry W. Strutz
Publisher:
Published: 1972
Total Pages: 84
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DOWNLOAD EBOOKAuthor: William I. Scallion
Publisher:
Published: 1999
Total Pages: 62
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DOWNLOAD EBOOKA 0.0196-scale model of the HL-20 lifting body, one of several configurations proposed for future crewed spacecraft, was tested in the Langley 31-Inch Mach 10 Tunnel. The purpose of the tests was to determine the effectiveness of fin-mounted elevons, a lower surface flush-mounted body flap, and a flush-mounted yaw controller at hypersonic speeds. The nominal angle-of-attack range, representative of hypersonic entry, was 20 to 41 degrees, the sideslip angles were 0, 2, and -2 degrees, and the test Reynolds number was 1.06 x 10[factor 6] based on model reference length. The aerodynamic, longitudinal, and lateral control effectiveness along with surface oil flow visualizations are presented and discussed. The configuration was longitudinally and laterally stable at the nominal center of gravity. The primary longitudinal control, the fin-mounted elevons, could not trim the model to the desired entry angle of attack of 30 degrees. The lower surface body flaps were effective for roll control and the associated adverse yawing moment was eliminated by skewing the body flap hinge lines. A yaw controller, flush-mounted on the lower surface, was also effective, and the associated small rolling moment was favorable.
Author:
Publisher:
Published: 1971
Total Pages: 292
ISBN-13:
DOWNLOAD EBOOKAuthor: Thomas C. Kelly
Publisher:
Published: 1962
Total Pages: 80
ISBN-13:
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