Search Results - Chu, Julio
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1
Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges
Published 1996Government Document Microfilm Book
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2
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
Published 1990Government Document Microfilm Book -
3
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° /
Published 1980Online Access
Online Access
Government Document eBook -
4
Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
Published 1996Online Access
Online Access
Government Document eBook -
5
High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Published 1990Other Authors: “…Chu, Julio…”
Government Document Microfilm Book -
6
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°
Published 1980Other Authors: “…Chu, Julio…”
Government Document Microfilm Book -
7
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊.
Published 1980Other Authors: “…Chu, Julio…”
Search for the full-text version of this title in HathiTrust
Government Document Book -
8
Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers /
Published 1992Other Authors: “…Chu, Julio…”
Search for the full-text version of this title in HathiTrust
Government Document Book -
9
Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
Published 1991Other Authors: “…Chu, Julio…”
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Government Document Microfilm Book