Read Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]

Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]

Lamb Milton.

4.9/5 (20071 ratings)

Description:We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]. To get started finding Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound], you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.

Pages: —

Format: PDF, EPUB & Kindle Edition

Publisher: —

Release: —

ISBN

Description: We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]. To get started finding Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound], you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.

Special Offer | $0.00

Special Offer! | $0.00

Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]

Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings Jr. 1974 [Leather Bound]

More Books

The Complete Harvard Classics - ALL 71 Volumes: The Five Foot Shelf & The Shelf of Fiction: The Famous Anthology of the Greatest Works of World Literature

The Complete Harvard Classics - ALL 71 Volumes: The Five Foot Shelf & The Shelf of Fiction: The Famous Anthology of the Greatest Works of World Literature

Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ / Milton Lamb and Robert L. Stallings Jr. ; Langley Researc [Leather Bound]

Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ / Milton Lamb and Robert L. Stallings Jr. ; Langley Researc [Leather Bound]

Integration effects of pylon geometry on a high-wing transport plane / John R. Carlson and Milton Lamb. 1989 [Leather Bound]

Integration effects of pylon geometry on a high-wing transport plane / John R. Carlson and Milton Lamb. 1989 [Leather Bound]

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds / Robert L. Stallings, and Milton Lamb. 1981 [Leather Bound]

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds / Robert L. Stallings, and Milton Lamb. 1981 [Leather Bound]

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / Robert L. Stallings, Jr., and Milton Lamb. 1980 [Leather Bound]

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / Robert L. Stallings, Jr., and Milton Lamb. 1980 [Leather Bound]

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 / Jerry M. Allen, Gloria Hernandez, and Milton Lamb. 1983 [Leather Bound]

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 / Jerry M. Allen, Gloria Hernandez, and Milton Lamb. 1983 [Leather Bound]

Sonic-boom characteristics in the extreme near field of a complex airplane model at mach numbers of 1.5 1.8 and 2.5 / by Odell A. Morris Milton Lamb and Harry W. Carlson. 1970 [Leather Bound]

Sonic-boom characteristics in the extreme near field of a complex airplane model at mach numbers of 1.5 1.8 and 2.5 / by Odell A. Morris Milton Lamb and Harry W. Carlson. 1970 [Leather Bound]

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements / Milton Lamb, [Leather Bound]

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements / Milton Lamb, [Leather Bound]

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 / Milton Lamb. 1981 [Leather Bound]

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 / Milton Lamb. 1981 [Leather Bound]