Low-speed aerodynamics : From wing theory to panel methods /

Introduction and background - Fundamentals of inviscid, incompressible flow - General solution of the incompressible, potential flow equations - Small-disturbance flow over three-dimensional wings: formulation of the problem - Small-disturbance flow over two-dimensional airfoils - Exact solutions wi...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autor principal: Katz, Joseph
Otros Autores: Plotkin, Allen
Formato: Libro
Lenguaje:Inglés
Publicado: New York : McGraw-Hill, 1991.
Colección:McGraw-Hill Series in Aeronautical and Aerospace Engineering
Materias:
AERODINAMICA
FLUJO INCOMPRESIBLE
FLUJO POTENCIAL
PERFILES AERODINAMICOS
Aporte de:Registro referencial: Solicitar el recurso aquí
Bibliotecas (ING-UNLP) de Universidad Nacional de La Plata
LEADER 01664Cam#a22002775a#4500
001 INGC-MON-019911
003 AR-LpUFI
005 20221019005911.0
008 190603s1991||||xxu|||||||||||||||||eng d
020 |a 0070504466 
040 |a AR-LpUFI  |b spa  |c AR-LpUFI 
080 |a 531.373.2 
100 1 |a Katz, Joseph.   |9 307025 
245 1 0 |a Low-speed aerodynamics :   |b From wing theory to panel methods /   |c Joseph Katz, Allen Plotkin. 
260 |a New York :   |b McGraw-Hill,   |c 1991. 
300 |a xiv, 632 p. :   |b il. 
490 |a McGraw-Hill Series in Aeronautical and Aerospace Engineering 
520 2 |a Introduction and background - Fundamentals of inviscid, incompressible flow - General solution of the incompressible, potential flow equations - Small-disturbance flow over three-dimensional wings: formulation of the problem - Small-disturbance flow over two-dimensional airfoils - Exact solutions with complex variables - Perturbation methods - Three-dimensional small disturbance solutions - Numerical (panel) methods - Singularity elements and influence coefficients - Two-dimensional numerical solutions - Three-dimensional numerical solutions - Unsteady incompressible potential flow - Enhancement of the potential flow model - Apendix - Airfoil integrals - Singularity distribution integrals - Principal value of the lifting-surface integral - Sample computer programs. 
650 4 |a AERODINAMICA  |9 268671 
650 4 |a FLUJO INCOMPRESIBLE  |9 264005 
650 4 |a FLUJO POTENCIAL  |9 274608 
650 4 |a PERFILES AERODINAMICOS  |9 280267 
700 1 |a Plotkin, Allen.  |9 307026 
929 |a 43054 DON Lugones (fotocopia) 
942 |c LIB  |6 _ 
999 |a SKV  |c 19910  |d 19910 

Ejemplares similares