| |
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9911074184303321 |
|
|
Titolo |
Increase of permanent public debt limit. May 9 (legislative day, April 30), 1984. -- Ordered to be printed |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
[Washington, D.C.] : , : [U.S. Government Printing Office], , 1984 |
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (15 pages) : tables |
|
|
|
|
|
|
Collana |
|
Senate report / 98th Congress, 2nd session. Senate ; ; no. 434 |
[United States congressional serial set] ; ; [serial no. 13558] |
|
|
|
|
|
|
|
|
Altri autori (Persone) |
|
DoleRobert J. <1923-2021> (Republican (KS)) |
GrassleyCharles (Republican (IA)) |
|
|
|
|
|
|
|
|
Soggetti |
|
Debts, Public |
Legislative materials. |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
Appendix, p. 8. |
Additional views of Mr. Grassley, p. 15. |
Batch processed record: Metadata reviewed, not verified. Some fields updated by batch processes. |
FDLP item number not assigned. |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
2. |
Record Nr. |
UNINA9911154454703321 |
|
|
Titolo |
Numerical methods for engine-airframe integration / / edited by S.N.B. Murthy, Gerald C. Paynter |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
|
|
|
|
|
|
|
|
|
ISBN |
|
1-60086-576-3 |
1-60086-357-4 |
|
|
|
|
|
|
|
|
Edizione |
[1st ed.] |
|
|
|
|
|
Descrizione fisica |
|
1 online resource (555 p.) |
|
|
|
|
|
|
Collana |
|
Progress in astronautics and aeronautics ; ; v. 102 |
|
|
|
|
|
|
Altri autori (Persone) |
|
MurthyS. N. B |
PaynterGerald C |
|
|
|
|
|
|
|
|
Disciplina |
|
|
|
|
|
|
|
|
Soggetti |
|
Airframes - Design and construction |
Airplanes - Motors |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"Technical papers selected from the AIAA 22nd Aerospace Sciences Meeting, January 1984, subsequently revised for this volume, and papers especially invited by the editors for this volume." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references and index. |
|
|
|
|
|
|
Nota di contenuto |
|
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation"" |
""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle |
|
|
|
|
|
|
|
|
|
|
Integration"" |
""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" |
|
|
|
|
|
| |