Aerodynamic characteristics of a wedge and cone at hypersonic Mach numbers.

Aerodynamic characteristics of a wedge and cone at hypersonic Mach numbers.

Saved in:

Bibliographic Details
Author / Creator:	Scherer, Lee R.
Imprint:	1950.
Description:	ix, 40 l. diagrs. 28 cm.
Language:	English
Subject:	Mach number Wedges Cone Cone. Mach number. Wedges.
Format:	Dissertations Print
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/3230278

Hidden Bibliographic Details
Varying Form of Title:	Hypersonic Mach numbers
Notes:	On cover: Guggenheim Aeronautical Laboratory, California Institute of Technology. Thesis--California Institute of Technology. Bibliography: leaf 18.

Similar Items

Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel /
by: Wilcox, Floyd J., Jr.
Published: (2013)

Hypersonic flows about a 25⁰ sharp cone /
by: Moss, James N.
Published: (2001)

Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ /
by: Loftin, Laurence K.
Published: (1954)

Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 /
by: Landrum, Emma Jean
Published: (1968)

Diffraction by wedges /
by: Budaev, Bair, 1954-
Published: (1995)

Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
by: Chu, Julio
Published: (1996)

Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement /
by: Glegg, Stewart A. L.
Published: (2017)

Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /
by: Thomas, Scott R.
Published: (1997)

Courant number and mach number insensitive CE/SE euler solvers /
by: Chang, Sin-Chung
Published: (2005)

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
by: Pittman, Jimmy L.
Published: (1980)

Effect of speed brakes on the supersonic aerodynamic characteristics of a variable-sweep tactical fighter model at Mach numbers from 1.60 to 2.50 /
by: Richardson, Celia S.
Published: (1968)

Experimental stagnation-point velocity gradients and heat-transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack /
by: Ellison, James C.
Published: (1969)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /
by: Re, Richard J.
Published: (1996)

Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 /
by: McGhee, Robert J.
Published: (1969)

DSMC simulation of separated flows about flared bodies at hypersonic conditions /
by: Moss, James N.
Published: (2000)

Precision wedge and bunker shots /
by: Fitzgerald, Jim, 1956-
Published: (1998)

The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /
by: Burbank, Paige B.
Published: (1953)

Aerodynamic effects of simulated ice accretion on a generic transport model /
Published: (2012)

Wedge-tailed eagle /
by: Olsen, Penny
Published: (2005)

Equivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations /
Published: (2011)

Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
Published: (1997)

Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
by: Laflin, Brenda E. Gile
Published: (1997)

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
Published: (1999)

Mechanics of thermal contraction cracks and ice-wedge polygons in permafrost.
by: Lachenbruch, Arthur H.
Published: (1962)

Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes /
by: Bobbitt, Percy J.
Published: (2012)

Wedge-tailed eagle /
by: Olsen, Penny
Published: (2005)

The woodwright's guide : working wood with wedge and edge /
by: Underhill, Roy
Published: (2008)

Tables for supersonic flow around right circular cones at zero angle of attack,
by: Sims, Joseph L.
Published: (1964)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /
by: Re, Richard J.
Published: (1996)

Diffraction by an immersed elastic wedge /
by: Croisille, Jean-Pierre, 1961-
Published: (1999)

Diffraction by an immersed elastic wedge /
by: Croisille, Jean-Pierre, 1961-
Published: (1999)

Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /
by: Hamilton, H. Harris
Published: (1968)

Airfoil section characteristics at high angles of attack /
by: Loftin, Laurence K.
Published: (1954)

Recent ice-wedge polygons in eastern Enontekiö, northernmost Finland.
by: Seppälä, Matti
Published: (1966)

Experimental measurements of sonic boom signatures using a continuous data acquisition technique /
by: Wilcox, Floyd J., Jr.
Published: (2013)

Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel /
by: Woodward, Richard P.
Published: (2012)

Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /
by: Erickson, Gary E.
Published: (2013)

Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /
by: Erickson, Gary E.
Published: (2013)

Research on supersonic inlet bleed /
by: Davis, David O.
Published: (2012)

English papier-mâché, its origin, development and decline,
by: Dickinson, George
Published: (1925)