Performance Summary And Analysis Of A Mach 30 Design Axisymmetric All External Compression Double Cone Inlet Mach Number Range 30 To 08
Download Performance Summary And Analysis Of A Mach 30 Design Axisymmetric All External Compression Double Cone Inlet Mach Number Range 30 To 08 full books in PDF, epub, and Kindle. Read online free Performance Summary And Analysis Of A Mach 30 Design Axisymmetric All External Compression Double Cone Inlet Mach Number Range 30 To 08 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Scientific and Technical Aerospace Reports
Author | : |
Publisher | : |
Total Pages | : 1282 |
Release | : 1982 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79
Author | : Owen H. Davis |
Publisher | : |
Total Pages | : 36 |
Release | : 1960 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
NASA Scientific and Technical Reports
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 966 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 956 |
Release | : 1970 |
Genre | : Science |
ISBN | : |
A Selected Listing of NASA Scientific and Technical Reports
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 962 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Aeroacoustics of Flight Vehicles
Author | : Harvey H. Hubbard |
Publisher | : |
Total Pages | : 620 |
Release | : 1991 |
Genre | : Aerodynamic noise |
ISBN | : |
Hypersonic Curved Compression Inlet and Its Inverse Design
Author | : Kunyuan Zhang |
Publisher | : Springer Nature |
Total Pages | : 340 |
Release | : 2020-01-22 |
Genre | : Science |
ISBN | : 9811507279 |
This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic–hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author’s research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.
Intake Aerodynamics
Author | : J. Seddon |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 440 |
Release | : 1999 |
Genre | : Science |
ISBN | : |
"Intake Aerodynamics, Second Edition" presents computational advancements and discoveries in intake aerodynamics. A companion volume to "Practical Intake Aerodynamic Design," this important text considers the problem of airflow, both internal and external to air intake, as applied to civil and military aircraft. It covers the aerodynamics of subsonic and supersonic intakes in real flows, maintaining a progression through the transonic range. Also considered is the joint perspective of the airframe designer and the propulsion specialist in practical cases. Readers will gain insight into the fluid mechanics behind the deceleration of air from free stream to engine velocity, and an understanding of air compression and external drag in extensively revised chapters reflecting progress in the field. More than 300 drawings and diagrams help to illustrate the points defined throughout the book. Copublished with Blackwell Science Ltd. Outside the United States and Canada, order from Blackwell Science Ltd., United Kingdom, tel 44 1865 206 206.
Hypersonic Airbreathing Propulsion
Author | : William H. Heiser |
Publisher | : AIAA |
Total Pages | : 632 |
Release | : 1994 |
Genre | : Science |
ISBN | : 9781563470356 |
An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR