Start Over
You searched for: author_facet Mack, Robert J.

Search Results

Cover image for An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts

An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts

Location
Access Content Online
Cover image for Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds

Location
Access Content Online
Cover image for A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport

A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport

Location
Access Content Online
Cover image for Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds

Location Call # Status
Joyner - Microforms B300 NAS 1.15:209534 ✔ Available
Cover image for A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport

A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport

Location Call # Status
Joyner - Microforms B300 NAS 1.15:209535 ✔ Available
Cover image for Experimental and theoretical study of flow fields around ducted-nacelle models

Experimental and theoretical study of flow fields around ducted-nacelle models

Location
Access Content Online
Cover image for Experimental and theoretical study of flow fields around ducted-nacelle models

Experimental and theoretical study of flow fields around ducted-nacelle models

Location Call # Status
Joyner - Microforms B300 NAS 1.15:207683 ✔ Available
Cover image for A methodology for designing aircraft to low sonic boom constraints

A methodology for designing aircraft to low sonic boom constraints

Location Call # Status
Joyner - Microforms B300 NAS 1.15:4246 ✔ Available
Cover image for A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas

A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas

Location Call # Status
Joyner - Microforms B300 NAS 1.15:4228 ✔ Available