Download or read book The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3 written by and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of a Blunt Half cone Entry Configuration with Horizontal Landing Capability written by and published by . This book was released on 1964 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
- Author :
- Publisher :
- Release : 1962
- ISBN :
- Pages : 96 pages
Characteristics of a Blunt Half cone Entry Configuration at Mach Numbers from 10 9 to 21 2 in Helium
Download or read book Characteristics of a Blunt Half cone Entry Configuration at Mach Numbers from 10 9 to 21 2 in Helium written by and published by . This book was released on 1962 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of a Blunt Half cone Entry Configuration at Mach Numbers of 5 2 7 4 and 10 4 written by and published by . This book was released on 1963 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of a Blunt Half cone Entry Configuration at Mach Numbers from 3 to 6 written by Michael F. Sarabia and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Variable geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control written by Roger H. Fournier and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Download or read book Large scale Wind tunnel Investigation of an M1 L Lifting Body with an Inflatable and a Rigid Afterbody written by Kenneth W. Mort and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Preliminary Investigation of Modified Blunt 13 Half cone Re entry Configurations at Subsonic Speeds written by George C. Kenyon and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 760 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Determination of Aerodynamic Drag on a Blunted 10 deg Cone at Angles of Attack in Hypersonic Rarefied Flow written by David E. Boylan and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 1346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight determined Low speed Lift and Drag Characteristics of the Lightweight M2 F1 Lifting Body written by Victor W. Horton and published by . This book was released on 1965 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF CONE AT MACH NUMBERS TO 0 92 written by and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Landing Point Control of Re entry Vehicles Utilizing Variable Area Aerodynamic Decelerators Incorporating Lift written by Avco-Everett Research Laboratory and published by . This book was released on 1962 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half cone Lifting body Configuration Having Deployable Horizontal Tails with Or Without Variable sweep Wings written by and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Angle of Attack and Bluntness on Laminar Heating rate Distributions of a 15 cone at a Mach Number of 10 6 written by Joseph W. Cleary and published by . This book was released on 1969 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar heating rate from wind tunnel tests using angle of attack and Reynolds number.