Search — EtoBox

7 works shown

5 duplicate copies folded into their books

Showing the first matches. Checking the full catalogue…

Books

12 files

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / Francis J. Capone, E. Ann Bare, Dorothy Arbiter.

Francis J. Capone

1986

Experimental Determination of Equivalent Solid Bodies to Represent Jets Exhausting into a Mach 2.20 External Stream / Lawrence E. Putnam and Francis J. Capone.

Lawrence E. Putnam

1969

Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel / David G. Evans, Keith A. Furgalus, and Francis S. Stepka.

David G. Evans

1970

Multiaxis Control Power from Thrust Vectoring for a Supersonic Fighter Aircraft Model at Mach 0.20 to 2.47 / Francis J. Capone and E. Ann Bare.

Francis J. Capone

1987

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 / Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.

Francis J. Capone

1991

Espaces et déplacements dans une écriture contemporaine non sédentaire

Adeline Liébert

PDF4.3 MB

Mack family

Julian Ellis Mack

1961

More matches

More books matching “Francois Mach”

Each book appears once. Open one to see all its editions and formats.

5 books so far

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 / George T. Carson, Jr., Francis J. Capone, and Mary L. Mason.

George T. Carson

1984

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 / Richard J. Re and Francis J. Capone.

Richard J. Re

1978

Performance of Twin Two-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 / Francis J. Capone and Donald L. Maiden.

Francis J. Capone

1977

Un Professeur de mathématiques à l'Université de Caen au commencement du XVIIe siècle

Henri (1867-1933) Prentout

PDF5.8 MB

Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925 / James B. Delano and Francis G. Morgan, Jr.

James B. Delano

1949

Genres

Books

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / Francis J. Capone, E. Ann Bare, Dorothy Arbiter.

Experimental Determination of Equivalent Solid Bodies to Represent Jets Exhausting into a Mach 2.20 External Stream / Lawrence E. Putnam and Francis J. Capone.

Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel / David G. Evans, Keith A. Furgalus, and Francis S. Stepka.

Multiaxis Control Power from Thrust Vectoring for a Supersonic Fighter Aircraft Model at Mach 0.20 to 2.47 / Francis J. Capone and E. Ann Bare.

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 / Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.

Espaces et déplacements dans une écriture contemporaine non sédentaire

Mack family

More books matching “Francois Mach”

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 / George T. Carson, Jr., Francis J. Capone, and Mary L. Mason.

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 / Richard J. Re and Francis J. Capone.

Performance of Twin Two-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 / Francis J. Capone and Donald L. Maiden.

Un Professeur de mathématiques à l'Université de Caen au commencement du XVIIe siècle

Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925 / James B. Delano and Francis G. Morgan, Jr.

Genres

Genres

Books

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / Francis J. Capone, E. Ann Bare, Dorothy Arbiter.

Experimental Determination of Equivalent Solid Bodies to Represent Jets Exhausting into a Mach 2.20 External Stream / Lawrence E. Putnam and Francis J. Capone.

Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel / David G. Evans, Keith A. Furgalus, and Francis S. Stepka.

Multiaxis Control Power from Thrust Vectoring for a Supersonic Fighter Aircraft Model at Mach 0.20 to 2.47 / Francis J. Capone and E. Ann Bare.

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 / Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.

Espaces et déplacements dans une écriture contemporaine non sédentaire

Mack family

More books matching “Francois Mach”

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 / George T. Carson, Jr., Francis J. Capone, and Mary L. Mason.

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 / Richard J. Re and Francis J. Capone.

Performance of Twin Two-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects at Speeds Up to Mach 2.20 / Francis J. Capone and Donald L. Maiden.

Un Professeur de mathématiques à l'Université de Caen au commencement du XVIIe siècle

Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925 / James B. Delano and Francis G. Morgan, Jr.