EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 swept Delta Wing

Download or read book Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 swept Delta Wing written by Louis E. Clark and published by . This book was released on 1977 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach Numbers from 0 33 to 1 20 of a Wing body Design Concept for a Hypersonic Research Airplane

Download or read book Aerodynamic Characteristics at Mach Numbers from 0 33 to 1 20 of a Wing body Design Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1977 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach Numbers from 0 33 to 1 20 of Wing body Design Concept for a Hypersonic Research Airplane

Download or read book Aerodynamic Characteristics at Mach Numbers from 0 33 to 1 20 of Wing body Design Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1977 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 Degrees Swept Delta Wing

Download or read book Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 Degrees Swept Delta Wing written by Louis E. Clark and published by . This book was released on 1977 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics Including Effect of Body Shape of a Mach 6 Aircraft Concept

Download or read book Aerodynamic Characteristics Including Effect of Body Shape of a Mach 6 Aircraft Concept written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-14 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Longitudinal aerodynamic characteristics for a hydrogen-fueled hypersonic transport concept at Mach 6 are presented. The model components consist of four bodies with identical longitudinal area distributions but different cross-sectional shapes and widths, a wing, horizontal and vertical tails, and a set of wing-mounted nacelles simulated by slid bodies on the wing upper surface. Lift-drag ratios were found to be only sightly affected by fuselage planform width or cross sectional shape. Relative distribution of fuselage volume above and below the wing was found to have an effect on the lift-drag ratio, with a higher lift drag ratio produced by the higher wing position. Riebe, G. D. Langley Research Center NASA-TP-2235, L-15675, NAS 1.60:2235 RTOP 505-43-23-10...

Book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 swept Double delta Wing at Mach Number 0 2

Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 swept Double delta Wing at Mach Number 0 2 written by Jim A. Penland and published by . This book was released on 1978 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach 6 of a Wing body Concept for a Hypersonic Research Airplane

Download or read book Aerodynamic Characteristics at Mach 6 of a Wing body Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1978 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed research airplane were investigated in the Langley 20 inch Mach six tunnel. The investigation consisted of configuration buildup from the basic body by adding a wing, center vertical tail, three-module scramjet, and six-module scramjet engine. The test Mach number was six at a Reynolds number, based on model fuselage length, of about 13,700,000. The test angle-of-attack range was 4 to 20 D at constant angles of sideslip of 0, 2, and 4 deg. The elevons were deflected from 10 to -15 D for pitch control. Roll and yaw control were investigated. Experimental aerodynamic characteristics are compared with analytical elements.

Book The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat top Hypersonic Aircraft at Mach Numbers from 0 6 to 1 4

Download or read book The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat top Hypersonic Aircraft at Mach Numbers from 0 6 to 1 4 written by Stuart L. Treon and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 swept Double delta Wing at Mach Numbers from 0 80 to 1 20 with Summary of Data from 0 20 to 6 0

Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 swept Double delta Wing at Mach Numbers from 0 80 to 1 20 with Summary of Data from 0 20 to 6 0 written by Jim A. Penland and published by . This book was released on 1979 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of a Hypersonic Cruise Aircraft Concept with Wing mounted Propulsion Systems at Mach Numbers of 2 96 3 96 and 4 63

Download or read book Aerodynamic Characteristics of a Hypersonic Cruise Aircraft Concept with Wing mounted Propulsion Systems at Mach Numbers of 2 96 3 96 and 4 63 written by Gregory D. Riebe and published by . This book was released on 1981 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: