Download or read book Wind tunnel Investigation of the Aerodynamic Pressures on the Apollo Command Module Configuration written by William C. Moseley and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel study of aerodynamic pressures on Apollo command module configuration.
Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics Determined During Development of the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1969 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0 30 to 1 20 written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle written by William C. Moseley (Jr.) and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale Wind tunnel Investigation of the Low speed Static Aerodynamic Characteristics of a Model of a Reentry Capsule written by William I. Scallion and published by . This book was released on 1959 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Investigation at Mach Numbers from 0 20 to 1 17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule written by Albin O. Pearson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive cylinder Model at Mach Numbers 1 75 to 4 50 written by Neil Arthur Zarin and published by . This book was released on 1964 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 0 40 to 1 14 of the Static Aerodynamic Characteristics of a Nonlifting Vehicle Suitable for Reentry written by Albin O. Pearson and published by . This book was released on 1959 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale Wind tunnel Investigation of the Low speed Static Aerodynamic Characteristics of a Model of a Reentry Capsule written by and published by . This book was released on 1959 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Wind Tunnel Measurements of Hysteresis in the Static Aerodynamic Characteristics of Aircraft written by J. F. Herman and published by . This book was released on 1979 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0 25 to 2 written by and published by . This book was released on 1975 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Investigation at Supersonic Speeds of the Lift Drag Static Stability and Control Characteristics of a 0 03 Scale Model of an Interim Development Version of the B 70 Airplane written by James C. Daugherty and published by . This book was released on 1961 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 0 8 to 1 4 of Static Longitudinal and Lateral directional Characteristics of an Unswept wing Airplane Model written by James L. Summers and published by . This book was released on 1956 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Results of the Aerodynamic Performance of a 1 8 Scale Model of a Twin Engine Transport with Multi Element Wing written by and published by . This book was released on 1997 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Results of the Aerodynamic Performance of a 1 8 Scale Model of a Twin Engine Transport with Multi Element Wing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was performed in the 14- by 22-Foot Subsonic Tunnel on a pressure instrumented 1/8-scale twin-engine subsonic transport to better understand the flow physics on a multi-element wing section. The wing consisted of a part-span, triple-slotted trailing edge flap, inboard leading-edge Krueger flap and an outboard leading-edge slat. The model was instrumented with flush pressure ports at the fuselage centerline and seven spanwise wing locations. The model was tested in cruise, take-off and landing configurations at dynamic pressures and Mach numbers from 10 lbf/ft(exp 2) to 50 lbf/ft(exp 2) and 0.08 to 0.17, respectively. This resulted in corresponding Reynolds numbers of 0.8 x 10(exp 5) to 1.8 x 10(exp 6). Pressure data were collected using electronically scanned pressure devices and force and moment data were collected with a six component strain gauge balance. Results are presented for various control surface deflections over an angle-of-attack range from -4 degrees to 16 degrees and sideslip angle range from -10 degrees to 10 degrees. Longitudinal and lateral directional aerodynamic data are presented as well as chordwise pressure distributions at the seven spanwise wing locations and the fuselage centerline. Laflin, Brenda E. Gile and Applin, Zachary T. and Jones, Kenneth M. Langley Research Center WIND TUNNEL TESTS; PRESSURE DISTRIBUTION; SUBSONIC SPEED; WINGS; REYNOLDS NUMBER; ANGLE OF ATTACK; MACH NUMBER; AERODYNAMIC CHARACTERISTICS; SIDESLIP; SCALE MODELS; TRAILING EDGE FLAPS; LEADING EDGES; STRAIN GAGE BALANCES; CONTROL SURFACES; TAKEOFF; AIRCRAFT LANDING; DYNAMIC PRESSURE; LATERAL STABILITY; LONGITUDINAL STABILITY...
