Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65

Download Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65 by :

Download or read book Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65 written by and published by . This book was released on 1961 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers

Download Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers by : Alvin Seiff

Download or read book Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers written by Alvin Seiff and published by . This book was released on 1961 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback

Download Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback by : Charles T. D'Aiutolo

Download or read book Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback written by Charles T. D'Aiutolo and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86

Download Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 by : William John Small

Download or read book Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 written by William John Small and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2

Download Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2 by :

Download or read book Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2 written by and published by . This book was released on 1964 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 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 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis 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 by : Stuart L. Treon

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:

Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6

Download Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 by : Walter P. Nelms

Download or read book Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 written by Walter P. Nelms and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The configuration had a delta planform with an elliptic cone forebody and an afterbody of elliptic cross section. Detailed effects of varying angle of attack (-2 to 15 deg), angle of sideslip (-2 to 8 deg), Mach number, and configuration buildup were considered. In addition, the effectiveness of horizontal tail, vertical tail, and canard stabilizing and control surfaces was investigated. The results indicate that all configurations were longitudinally stable near maximum lift drag ratio. The configurations with vertical tails were directionally stable at all angles of attack. Trim penalties were small at hypersonic speeds for a center of gravity location representative of the airplane, but because of the large rearward travel of the aerodynamic center, trim penalties were severe at transonic Mach numbers.

Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6

Download Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 by : James C. Ellison

Download or read book Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 written by James C. Ellison and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Also available online.

Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01

Download Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01 by : Gerald V. Foster

Download or read book Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01 written by Gerald V. Foster and published by . This book was released on 1959 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack Up to 90 Degrees for a Range of Reynolds Numbers

Download Low-speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack Up to 90 Degrees for a Range of Reynolds Numbers PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Low-speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack Up to 90 Degrees for a Range of Reynolds Numbers by : James S. Bowman

Download or read book Low-speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack Up to 90 Degrees for a Range of Reynolds Numbers written by James S. Bowman and published by . This book was released on 1960 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack

Download An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack by : Robert H. Feldhuhn

Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack written by Robert H. Feldhuhn and published by . This book was released on 1968 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.

Hypersonic Free Flight Research: Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf

Download Hypersonic Free Flight Research: Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Hypersonic Free Flight Research: Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf by :

Download or read book Hypersonic Free Flight Research: Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf written by and published by . This book was released on 1960 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6

Download Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6 by : J. T. Best (Jr.)

Download or read book Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1.5 to 5.6 written by J. T. Best (Jr.) and published by . This book was released on 1975 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52

Download Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52 by :

Download or read book Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52 written by and published by . This book was released on 1964 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Measurement at Mach 19 for a Winged Re-entry Configuration

Download Pressure Measurement at Mach 19 for a Winged Re-entry Configuration PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Pressure Measurement at Mach 19 for a Winged Re-entry Configuration by : Stavros A. Hartofilis

Download or read book Pressure Measurement at Mach 19 for a Winged Re-entry Configuration written by Stavros A. Hartofilis and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane

Download Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane by : James L. Dillon

Download or read book Aerodynamic Characteristics at Mach Number 0.2 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 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds

Download Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds by :

Download or read book Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds written by and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: