Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50
Author: George H. Holdaway
Publisher:
Published: 1960
Total Pages: 70
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: George H. Holdaway
Publisher:
Published: 1960
Total Pages: 70
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1960
Total Pages: 66
ISBN-13:
DOWNLOAD EBOOKAuthor: George H. Holdaway
Publisher:
Published: 1960
Total Pages: 82
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1960
Total Pages: 77
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1960
Total Pages: 76
ISBN-13:
DOWNLOAD EBOOKAuthor: George H. Holdaway
Publisher:
Published: 1961
Total Pages: 80
ISBN-13:
DOWNLOAD EBOOKAuthor: George H. Holdaway
Publisher:
Published: 1960
Total Pages: 76
ISBN-13:
DOWNLOAD EBOOKAuthor: Library of Congress Science and Technology Division
Publisher:
Published: 1962
Total Pages: 252
ISBN-13:
DOWNLOAD EBOOKAuthor: Edward J. Hopkins
Publisher:
Published: 1967
Total Pages: 98
ISBN-13:
DOWNLOAD EBOOKAuthor: W. F. Lindsey
Publisher:
Published: 1954
Total Pages: 24
ISBN-13:
DOWNLOAD EBOOKAbstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.