Author : Anonim
Publisher : Unknown
Page : 418 pages
File Size : 45,5 Mb
Release : 1974
Category : Electronic
ISBN : MINN:31951000846486N
Flight Evaluation Of Hl 10 Lifting Body Handling Qualities At Mach Numbers From 0 30 To 1 86
Flight Evaluation Of Hl 10 Lifting Body Handling Qualities At Mach Numbers From 0 30 To 1 86 Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Flight Evaluation Of Hl 10 Lifting Body Handling Qualities At Mach Numbers From 0 30 To 1 86 book. This book definitely worth reading, it is an incredibly well-written.
Flight Evaluation of HL-10 Lifting Body Handling Qualities at Mach Numbers from 0.30 to 1.86
Author : Robert W. Kempel,John A. Manke
Publisher : Unknown
Page : 52 pages
File Size : 40,9 Mb
Release : 1974
Category : Aerodynamics
ISBN : UIUC:30112106749705
Flight Evaluation of HL-10 Lifting Body Handling Qualities at Mach Numbers from 0.30 to 1.86 by Robert W. Kempel,John A. Manke Pdf
Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air
Author : William I. Scallion
Publisher : Unknown
Page : 62 pages
File Size : 51,8 Mb
Release : 1999
Category : Airplanes
ISBN : NASA:31769000633209
Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air by William I. Scallion Pdf
A 0.0196-scale model of the HL-20 lifting body, one of several configurations proposed for future crewed spacecraft, was tested in the Langley 31-Inch Mach 10 Tunnel. The purpose of the tests was to determine the effectiveness of fin-mounted elevons, a lower surface flush-mounted body flap, and a flush-mounted yaw controller at hypersonic speeds. The nominal angle-of-attack range, representative of hypersonic entry, was 20 to 41 degrees, the sideslip angles were 0, 2, and -2 degrees, and the test Reynolds number was 1.06 x 10[factor 6] based on model reference length. The aerodynamic, longitudinal, and lateral control effectiveness along with surface oil flow visualizations are presented and discussed. The configuration was longitudinally and laterally stable at the nominal center of gravity. The primary longitudinal control, the fin-mounted elevons, could not trim the model to the desired entry angle of attack of 30 degrees. The lower surface body flaps were effective for roll control and the associated adverse yawing moment was eliminated by skewing the body flap hinge lines. A yaw controller, flush-mounted on the lower surface, was also effective, and the associated small rolling moment was favorable.
Lift and Drag Characteristics of the HL-10 Lifting Body During Subsonic Gliding Flight
Author : Jon S. Pyle
Publisher : Unknown
Page : 36 pages
File Size : 47,9 Mb
Release : 1971
Category : Drag (Aerodynamics)
ISBN : UIUC:30112106881748
Lift and Drag Characteristics of the HL-10 Lifting Body During Subsonic Gliding Flight by Jon S. Pyle Pdf
Aero/space Engineering
Author : Anonim
Publisher : Unknown
Page : 872 pages
File Size : 46,6 Mb
Release : 1960-07
Category : Aeronautics
ISBN : CORNELL:31924058348156
Aero/space Engineering by Anonim Pdf
Wingless Flight
Author : R. Dale Reed,Darlene Lister
Publisher : University Press of Kentucky
Page : 256 pages
File Size : 55,5 Mb
Release : 2014-07-15
Category : Technology & Engineering
ISBN : 9780813161600
Wingless Flight by R. Dale Reed,Darlene Lister Pdf
Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 532 pages
File Size : 51,7 Mb
Release : 1971
Category : Aeronautics
ISBN : UFL:31262082069286
Scientific and Technical Aerospace Reports by Anonim Pdf
Interavia
Author : Anonim
Publisher : Unknown
Page : 688 pages
File Size : 44,7 Mb
Release : 1957
Category : Aeronautics
ISBN : UOM:39015011167114
Interavia by Anonim Pdf
Government Reports Announcements & Index
Author : Anonim
Publisher : Unknown
Page : 1020 pages
File Size : 44,6 Mb
Release : 1986-07
Category : Science
ISBN : CORNELL:31924055269934
Government Reports Announcements & Index by Anonim Pdf
Applied Science & Technology Index
Author : Anonim
Publisher : Unknown
Page : 1480 pages
File Size : 46,5 Mb
Release : 1969
Category : Electronic journals
ISBN : UCAL:$B405737
Applied Science & Technology Index by Anonim Pdf
International Aerospace Abstracts
Author : Anonim
Publisher : Unknown
Page : 936 pages
File Size : 54,5 Mb
Release : 1993
Category : Aeronautics
ISBN : STANFORD:36105016617198
International Aerospace Abstracts by Anonim Pdf
Aeroacoustics of Flight Vehicles
Author : Harvey H. Hubbard
Publisher : Unknown
Page : 620 pages
File Size : 53,8 Mb
Release : 1991
Category : Aerodynamic noise
ISBN : STANFORD:36105024722329
Aeroacoustics of Flight Vehicles by Harvey H. Hubbard Pdf
Mach 3+
Author : Peter W. Merlin
Publisher : Unknown
Page : 0 pages
File Size : 47,6 Mb
Release : 2002
Category : Aerodynamics, Hypersonic
ISBN : OCLC:773209913
Mach 3+ by Peter W. Merlin Pdf
"During the 1950s, American aircraft designers emphasized configurations that flew increasingly high and fast, a trend that continued for nearly two decades. Then, during the 1070s, efficiency, noise reduction, and fuel economy also became important considerations, in part because military analysts no longer deemed speed and altitude the paramount capabilities necessary to ensure national security. Among the aircraft designs that transitioned from paper to hardware during the high-speed era, the Lockheed Blackbirds hold a unique place. The A-12, YF-12A, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. To this day, they remain the only production aircraft capable of sustained cruise in excess of Mach 3. Developed in utmost secrecy, they eventually became some of the world's most famous aircraft. Conceived originally as spyplanes, several Blackbirds saw service with the National Aeronautics and Space Administration (NASA) as research platforms. This monograph describes the first major NASA project involving the Blackbirds. Conducted with the U.S. Air Force (USAF) as a partner, the NASA/USAF YF-12 research lasted 10 years, and produced a wealth of data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft."--Preface.
Flying beyond the stall
Author : Douglas A. Joyce
Publisher : Unknown
Page : 409 pages
File Size : 52,9 Mb
Release : 2014
Category : Research aircraft
ISBN : 1626830193
Flying beyond the stall by Douglas A. Joyce Pdf
The X-31 Enhanced Fighter Maneuverability Demonstrator was unique among experimental aircraft. A joint effort of the United States and Germany, the X-31 was the only X-plane to be designed, manufactured, and flight tested as an international collaboration. It was also the only X-plane to support two separate test programs conducted years apart, one administered largely by NASA and the other by the U.S. Navy, as well as the first X-plane ever to perform at the Paris Air Show. Flying Beyond the Stall begins by describing the government agencies and private-sector industries involved in the X-31 program, the genesis of the supermaneuverability concept and its initial design breakthroughs, design and fabrication of two test airframes, preparation for the X-31's first flight, and the first flights of Ship #1 and Ship #2. Subsequent chapters discuss envelope expansion, handling qualities (especially at high angles of attack), and flight with vectored thrust. The book then turns to the program's move to NASA's Dryden Flight Research Center and actual flight test data. Additional tasking, such as helmet-mounted display evaluations, handling quality studies, aerodynamic parameter estimation, and a "tailless" study are also discussed.The book describes how, in the aftermath of a disastrous accident with Ship #1 in 1995, Ship #2 was prepared for its outstanding participation in the Paris Air Show. The aircraft was then shipped back to Edwards AFB and put into storage until the late 1990s, when it was refurbished for participation in the U. S. Navy's VECTOR program. The book ends with a comprehensive discussion of lessons learned and includes an Appendix containing detailed information.
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 296 pages
File Size : 42,7 Mb
Release : 1991
Category : Aeronautics
ISBN : MINN:30000005718709